{"id":354,"date":"2018-07-18T05:46:02","date_gmt":"2018-07-18T05:46:02","guid":{"rendered":"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/?post_type=chapter&#038;p=354"},"modified":"2019-05-15T12:03:21","modified_gmt":"2019-05-15T12:03:21","slug":"354","status":"publish","type":"chapter","link":"https:\/\/ebooks.inflibnet.ac.in\/itp12\/chapter\/354\/","title":{"rendered":"Mobile communications Satellite systems (Part-1)"},"content":{"raw":"<div><span style=\"float: right;\"><a href=\"https:\/\/youtu.be\/uIzBLF30nLI\" target=\"_blank\" rel=\"noopener\"><img src=\"http:\/\/epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/2018\/11\/download.png\" alt=\"epgp books\" width=\"75px\" height=\"75px;\" \/><\/a>\r\n<\/span><\/div>\r\n<strong>Learning Objectives<\/strong>\r\n<ul>\r\n \t<li>Communication satellite Segments<\/li>\r\n \t<li>History Satellite communication<\/li>\r\n \t<li>Classical Satellite Systems<\/li>\r\n \t<li>Applications<\/li>\r\n \t<li>Indian Communication Satellites and Critical Services<\/li>\r\n \t<li>Basics of Geo-stationary Satellites<\/li>\r\n \t<li>satellite Inclination angle<\/li>\r\n \t<li>Satellite Elevation Angle<\/li>\r\n \t<li>Propagation Loss<\/li>\r\n \t<li>Satellite Orbits<\/li>\r\n \t<li>GEO<\/li>\r\n \t<li>LEO<\/li>\r\n \t<li>MEO<\/li>\r\n \t<li>Frequency Bands, Spectrum<\/li>\r\n<\/ul>\r\n<p class=\"hanging-indent\"><strong>Introduction<\/strong><\/p>\r\n&nbsp;\r\n<p style=\"text-align: justify;\">Satellite communication supports the mobile communications. Satellites offer global coverage without wiring costs for base stations and are almost independent of varying population densities.<\/p>\r\n&nbsp;\r\n\r\n<img class=\"aligncenter size-full wp-image-358\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic1.png\" alt=\"\" width=\"253\" height=\"189\" \/>\r\n<p style=\"text-align: center;\"><strong>Figure 1<\/strong><\/p>\r\n&nbsp;\r\n<p class=\"hanging-indent\"><strong>Satellite Communication can be broadly divided in three segments<\/strong><\/p>\r\n&nbsp;\r\n\r\n<img class=\"aligncenter size-full wp-image-359\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic2.png\" alt=\"\" width=\"1014\" height=\"357\" \/>\r\n<p style=\"text-align: center;\"><strong>Figure 2 : Space Communication Segments<\/strong><\/p>\r\n\r\n<ol>\r\n \t<li style=\"text-align: justify;\">Space Segments: consists of mainly Communication satellites in various orbits GEO, LEO, MEO and HEO depending upon the application needs to the users<\/li>\r\n \t<li style=\"text-align: justify;\">Ground Segments: consists of mainly Hub or Gateway Earth Station user terminal.<\/li>\r\n \t<li style=\"text-align: justify;\">Communication Channel Communication is established by Up link and Down link frequency in UHF, L band, S-band, Normal C-band, Extended C-band, Ku-band, X-band, Ka-band, Q-band, V-band, W-band, Optical-bands etc. depending on the user application, approval by ITU, band width, Geographical location, data rate, data volume and traffic density requirements.<\/li>\r\n<\/ol>\r\n<p style=\"text-align: justify;\">The high speed of satellites with a low altitude raises new problems for routing, localization of mobile users, and handover of communication links.<\/p>\r\n&nbsp;\r\n<div>\r\n\r\n<strong>History Satellite communication<\/strong>\r\n\r\n&nbsp;\r\n<p style=\"text-align: justify;\">Satellite communication began after the Second World War. In 1945, Arthur C. Clarke published his essay on \u2018Extra Terrestrial Relays\u2019. But it was not until 1957, in the middle of the cold war, that the\u00a0 sudden launching of the first satellite SPUTNIK by the Soviet Union shocked the Western world. SPUTNIK is not at all comparable to a satellite today; it was basically a small sender transmitting a periodic \u2018beep\u2019.<\/p>\r\n&nbsp;\r\n<p style=\"text-align: justify;\">Today, geostationary satellites are the backbone of news broadcasting in the sky. Their great advantage is their fixed position in the sky. Their rotation is synchronous to the rotation of the earth, so they appear to be pinned to a certain location.<\/p>\r\n&nbsp;\r\n<p style=\"text-align: justify;\"><span style=\"font-size: 1em;\">The first commercial geostationary communication satellite INTELSAT 1 (also known as \u2018Early Bird\u2019) went into operation in 1965. It was in service for one-and-a-half years, weighed 68 kg and offered 240 duplex telephone channels or, alternatively, a single TV channel. INTELSAT 2 followed in 1967, INTELSAT- 3 in 1969 already offered 1,200 telephone channels. While communication on land always provides the alternative of using wires, this is not the case for ships at sea. Three MARISAT satellites went into operation in 1976 which offered worldwide maritime communication. However, Sender and receiver still had to be installed on the ships with large antennas (1.2 m antenna, 40 W transmit power). The first mobile satellite telephone system, INMARSAT-A, was introduced in 1982. Six years later, INMARSAT-C became the first satellite system to offer mobile phone and data services. (Data rates of about 600 bit\/s, interfaces to the X.25 packet data network exist.) In 1993, satellite telephone systems finally became fully digital with INMARSAT-M.<\/span><\/p>\r\n&nbsp;\r\n<p style=\"text-align: justify;\"><span style=\"font-size: 1em;\">Nineteen ninety-eight marked the beginning of a new age of satellite data communication with <\/span><span style=\"font-size: 1em;\">the introduction of global satellite systems for small mobile phones, such as, e.g., Iridium and Global star. There are more than 2000 geostationary satellites in commercial use which shows the impressive growth of satellite communication over the last 50 years.<\/span><\/p>\r\n&nbsp;\r\n<p style=\"text-align: justify;\"><span style=\"font-size: 1em;\">The Indian Space Program was started by 1969, by Great Visionary Dr.Vikram Sarabhai. The first Indian Satellite INSAT-1A was launched in 1981. Currently INSAT and GSAT series 42 satellites are operational in orbit.<\/span><\/p>\r\n\r\n<\/div>\r\n<p class=\"hanging-indent\" style=\"text-align: justify;\"><strong>Classical Satellite Systems<\/strong><\/p>\r\n&nbsp;\r\n<p style=\"text-align: justify;\">Earlier satellites were simple transponders; today\u2019s satellites rather resemble flying routers. Transponders basically receive a signal on one frequency, amplify the signal and transmit it on another frequency. While in the beginning only analog amplification was possible, the use of digital signals also allows for signal regeneration. The satellite decodes the signal into a bit stream, and codes it again into a signal. The advantage of digital regeneration compared to pure analog amplification is the higher quality of the received signal on the earth. Today\u2019s communication satellites provide many functions of higher communication layers, e.g., inter- satellite routing, error correction etc.<\/p>\r\n&nbsp;\r\n\r\n<img class=\"aligncenter size-full wp-image-360\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic3.png\" alt=\"\" width=\"573\" height=\"370\" \/>\r\n<p style=\"text-align: center;\"><strong>Figure 3 : Classical Satellite Systems<\/strong><\/p>\r\n&nbsp;\r\n<p style=\"text-align: justify;\">Figure 3 shows a classical scenario for satellite systems supporting global mobile communication. Depending on its type, each satellite can cover a certain area on the earth with its beam (the so-called \u2018footprint\u2019. Within the footprint, communication with the satellite is possible for mobile users via a <strong>mobile user link (MUL) <\/strong>and for the base station controlling the satellite and acting as gateway to other networks via the <strong>gateway link (GWL)<\/strong>. Satellites may be able to communicate directly with each other via <strong>i<\/strong><strong>ntersatellite links (ISL)<\/strong>.<\/p>\r\n&nbsp;\r\n\r\n<img class=\"aligncenter wp-image-361 size-full\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic4.png\" alt=\"\" width=\"892\" height=\"373\" \/>\r\n<p style=\"text-align: center;\"><strong>Figure 4 : Communication Satellites - Intersatellite Link (ISL).<\/strong><\/p>\r\n&nbsp;\r\n<p style=\"text-align: justify;\"><span style=\"text-align: justify; font-size: 1em;\">This facilitates direct communication between users within different footprints without using base stations or other networks on earth. Saving extra links from satellite to earth can reduce latency for data packets and voice data. Some satellites have special antennas to create smaller cells using spot beams (e.g., 163 spot beams per satellite in the ICO system (ICO, 2002)). The required terrestrial service infrastructure for satellite control and the control links between. Satellite systems will continue to be, a valuable addition to the many networks already in existence on earth. Users might communicate using ISDN or other PSTN, even cellular networks\u00a0<\/span><span style=\"text-align: initial; font-size: 1em;\">such as\u00a0 GSM and UMTS. Many\u00a0 gateways provide seamless communication between these different networks. A real challenge, for example, is the smooth, seamless handover between a cellular network and a satellite system (vertical handover) as it is already well known from within cellular networks (horizontal handover). Users should not notice the switching from, e.g., GSM, to a satellite network during conversation.<\/span><\/p>\r\n\r\n<div>\r\n<ul>\r\n \t<li style=\"text-align: justify;\"><strong>Applications \u00a0<\/strong>Traditionally, satellites have been used in the following areas:<\/li>\r\n \t<li style=\"text-align: justify;\"><strong>Weather forecasting: <\/strong>Satellites are used to capture picture of the earth and relay on ground station to predict the weather conditions. It is very useful to predict anomalies like Hurricane beforehand so that preventive measures can be taken,<\/li>\r\n \t<li style=\"text-align: justify;\"><strong>R<\/strong><strong>a<\/strong><strong>dio and TV broadcast satellites: <\/strong>Satellites and easy and cheap alternative to cable network for radio and television broadcasting.<\/li>\r\n \t<li style=\"text-align: justify;\"><strong>Military satellites: C<\/strong>ommunication links managed through satellite because they are safer from attack by enemies Most of the Military satellites operate on X-band.<\/li>\r\n \t<li style=\"text-align: justify;\"><strong>Satellites for navigation: <\/strong>The global positioning system (GPS) provides precise localization information with high precision of few meters. All ships and aircraft use GPS for their navigation systems. Information obtained from GPS receivers installed in vehicles is used for fleet management localization of vehicles etc. The Indian Space Research Organization (ISRO) has developed indigenous Indian Regional Navigation Satellite System called \u201cNavIC\u201d as deshi GPS with 7 GEO\/GSO satellites. It has become operational. It can replace the most popular GPS of US, Glonass of Russia, Beidou of China or Galileo of European. NavIC System can develop potential application for Road Navigation, Rail Navigation and safety, Generate warning for unmanned Level Crossing, Vessel Monitoring and Tracking for costal Surveillance, Surveying \u2013Land, Marine, Differential correction with Geodetic Receivers, Disaster management and warning, Emergency Calling, Location based services, Ionospheric monitoring and scintillation studies, Time and Frequency synchronization for Internet and Intranet application and several applications for Scientific and Research communities and Services to society.<\/li>\r\n \t<li style=\"text-align: justify;\"><strong>Global telephone backbones: <\/strong>Communication satellites are emerging as an alternative to cables for international telephone backbone .The satellites are increasingly being replaced by fiber optical cables crossing the oceans. The main reason for this is the tremendous capacity of fiber optical links (commercially some 10 Gbit\/s using wavelength division\u00a0<span style=\"text-align: initial; font-size: 1em;\">multiplexing, several Tbit\/s in labs) and, in particular, the much lower delay compared to satellites. While the signal to a geostationary satellite has to travel about 72,000 km from a sender via the satellite to the receiver, the distance is typically less than 10,000 km if a fiber-optical link crossing the Pacific or Atlantic Ocean is used. Unfortunately, the speed of light is limited, resulting in a one-way, single-hop time delay of 0.25 s for geostationary satellites. Using satellites for telephone conversation is sometimes annoying.<\/span><\/li>\r\n \t<li style=\"text-align: justify;\"><strong style=\"font-size: 1em;\">C<\/strong><strong style=\"font-size: 1em;\">onnections for remote or developing areas: <\/strong><span style=\"font-size: 1em;\">Satellites offer a simple and quick connection to global networks to the places which are inaccessible due to their geographical location.<\/span><\/li>\r\n \t<li style=\"text-align: justify;\"><strong style=\"text-align: initial; font-size: 1em;\">Global mobile communication: <\/strong><span style=\"text-align: initial; font-size: 1em;\">Most recent advantage of satellites is mobile data communication. Geostationary satellites are not ideal for this because of high latency rate therefore; there is need of satellites using using lower orbits. Use of satellites for mobile communication is not as a replacer but as an extension to existing systems. They have an edge over existing cellular systems such as AMPS and GSM because of world wide coverage. For the UMTS system frequency bands directly adjacent to the terrestrial bands have been allocated for the satellite segment (S-Band: 1980\u20132010 MHz uplink, 2170\u20132200 MHz downlink).<\/span><\/li>\r\n<\/ul>\r\n<\/div>\r\n<p style=\"text-align: justify;\"><strong>INDIAN Critical Services through Indigenous Communication Satellites<\/strong><\/p>\r\n&nbsp;\r\n\r\n<img class=\"aligncenter size-full wp-image-362\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic5.png\" alt=\"\" width=\"1008\" height=\"846\" \/>\r\n<p style=\"text-align: center;\"><strong>Figure 5 : Indian Critical Services via Communication Satellites.<\/strong><\/p>\r\n&nbsp;\r\n<p style=\"text-align: justify;\">India\u2019s INSAT and GSAT series of communication satellites are offering UHF, S-band Normal C band, Cext Cband, Ku-Band and Ka band multi band multipurpose Transponders for Telecommunication, Broadcasting, DTH, VSAT\/Business Communication Societal Development, Dedicated satellite for Tele-education, e-learning, Telemedicine, METSAT and Disaster services, mobile services, advance communication services for internet, high throughput satellite for more cannels and higher data rate and many more services for country\u2019s development program.<\/p>\r\n&nbsp;\r\n<p class=\"hanging-indent\"><strong>Indian Communication Satellites<\/strong><\/p>\r\n&nbsp;\r\n<p class=\"hanging-indent\"><strong>Table 1 :<\/strong><\/p>\r\n\r\n<table class=\"lines\" style=\"height: 1619px;\" border=\"1px solid black\" width=\"600\" align=\"center\">\r\n<tbody>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">SATELLITE<\/td>\r\n<td style=\"width: 74.0625px;\">Launch Date<\/td>\r\n<td style=\"width: 86.0625px;\">Launch Mass<\/td>\r\n<td style=\"width: 90.0625px;\">Launch Vehicle<\/td>\r\n<td style=\"width: 57.0625px;\">Orbit<\/td>\r\n<td style=\"width: 116.063px;\">Application<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">INSAT-3B<\/td>\r\n<td style=\"width: 74.0625px;\">Mar 22, 2000<\/td>\r\n<td style=\"width: 86.0625px;\">2,070 Kg<\/td>\r\n<td style=\"width: 90.0625px;\">Ariane-5G<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">INSAT-2E<\/td>\r\n<td style=\"width: 74.0625px;\">Apr 03, 1999<\/td>\r\n<td style=\"width: 86.0625px;\">2,550 Kg<\/td>\r\n<td style=\"width: 90.0625px;\">Ariane-42P H10-3<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">INSAT-2D<\/td>\r\n<td style=\"width: 74.0625px;\">Jun 04, 1997<\/td>\r\n<td style=\"width: 86.0625px;\">2079 Kg<\/td>\r\n<td style=\"width: 90.0625px;\">Ariane-44L H10-3<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">INSAT-2C<\/td>\r\n<td style=\"width: 74.0625px;\">Dec 07, 1995<\/td>\r\n<td style=\"width: 86.0625px;\">2106 Kg<\/td>\r\n<td style=\"width: 90.0625px;\">Ariane-44L H10-3<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">INSAT-2B<\/td>\r\n<td style=\"width: 74.0625px;\">Jul 23, 1993<\/td>\r\n<td style=\"width: 86.0625px;\">1906 kg<\/td>\r\n<td style=\"width: 90.0625px;\">Ariane-44L H10+<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">INSAT-2A<\/td>\r\n<td style=\"width: 74.0625px;\">Jul 10, 1992<\/td>\r\n<td style=\"width: 86.0625px;\">1906 kg<\/td>\r\n<td style=\"width: 90.0625px;\">Ariane-44L H10<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">INSAT-1D<\/td>\r\n<td style=\"width: 74.0625px;\">Jun 12, 1990<\/td>\r\n<td style=\"width: 86.0625px;\"><\/td>\r\n<td style=\"width: 90.0625px;\">Delta 4925<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">INSAT-1C<\/td>\r\n<td style=\"width: 74.0625px;\">Jul 22, 1988<\/td>\r\n<td style=\"width: 86.0625px;\"><\/td>\r\n<td style=\"width: 90.0625px;\">Ariane-3<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">INSAT-1B<\/td>\r\n<td style=\"width: 74.0625px;\">Aug 30, 1983<\/td>\r\n<td style=\"width: 86.0625px;\"><\/td>\r\n<td style=\"width: 90.0625px;\">Shuttle [PAM-D]<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">INSAT-1A<\/td>\r\n<td style=\"width: 74.0625px;\">Apr 10, 1982<\/td>\r\n<td style=\"width: 86.0625px;\"><\/td>\r\n<td style=\"width: 90.0625px;\">Delta<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">HAMSAT<\/td>\r\n<td style=\"width: 74.0625px;\">May 05, 2005<\/td>\r\n<td style=\"width: 86.0625px;\"><\/td>\r\n<td style=\"width: 90.0625px;\">PSLV-C6<\/td>\r\n<td style=\"width: 57.0625px;\">SSPO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">EDUSAT<\/td>\r\n<td style=\"width: 74.0625px;\">Sep 20, 2004<\/td>\r\n<td style=\"width: 86.0625px;\">1950.5 kg<\/td>\r\n<td style=\"width: 90.0625px;\">GSLV-F01<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">INSAT-3E<\/td>\r\n<td style=\"width: 74.0625px;\">Sep 28, 2003<\/td>\r\n<td style=\"width: 86.0625px;\">2,775 Kg<\/td>\r\n<td style=\"width: 90.0625px;\">Ariane5-V162<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">GSAT-2<\/td>\r\n<td style=\"width: 74.0625px;\">May 08, 2003<\/td>\r\n<td style=\"width: 86.0625px;\">1800 Kg<\/td>\r\n<td style=\"width: 90.0625px;\">GSLV-D2<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">INSAT-3A<\/td>\r\n<td style=\"width: 74.0625px;\">Apr 10, 2003<\/td>\r\n<td style=\"width: 86.0625px;\">2,950 Kg<\/td>\r\n<td style=\"width: 90.0625px;\">Ariane5-V160<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Climate &amp; Environm., Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">KALPANA-1<\/td>\r\n<td style=\"width: 74.0625px;\">Sep 12, 2002<\/td>\r\n<td style=\"width: 86.0625px;\">1060 Kg<\/td>\r\n<td style=\"width: 90.0625px;\">PSLV-C4<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Climate &amp; Environm. Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">INSAT-3C<\/td>\r\n<td style=\"width: 74.0625px;\">Jan 24, 2002<\/td>\r\n<td style=\"width: 86.0625px;\">2,650 Kg<\/td>\r\n<td style=\"width: 90.0625px;\">Ariane5-V147<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Climate &amp; Environ., Commun<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">GSAT-1<\/td>\r\n<td style=\"width: 74.0625px;\">Apr 18, 2001<\/td>\r\n<td style=\"width: 86.0625px;\">1530 Kg<\/td>\r\n<td style=\"width: 90.0625px;\">GSLV-D1<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">HAMSAT<\/td>\r\n<td style=\"width: 74.0625px;\">May 05, 2005<\/td>\r\n<td style=\"width: 86.0625px;\"><\/td>\r\n<td style=\"width: 90.0625px;\">PSLV-C6<\/td>\r\n<td style=\"width: 57.0625px;\">SSPO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">GSAT-12<\/td>\r\n<td style=\"width: 74.0625px;\">Jul 15, 2011<\/td>\r\n<td style=\"width: 86.0625px;\">1410 kg<\/td>\r\n<td style=\"width: 90.0625px;\">PSLV-C17<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">GSAT-8<\/td>\r\n<td style=\"width: 74.0625px;\">May 21, 2011<\/td>\r\n<td style=\"width: 86.0625px;\">3093 kg<\/td>\r\n<td style=\"width: 90.0625px;\">Ariane-5 VA-202<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication, Navigation<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">GSAT-5P<\/td>\r\n<td style=\"width: 74.0625px;\">Dec 25, 2010<\/td>\r\n<td style=\"width: 86.0625px;\">2310 kg<\/td>\r\n<td style=\"width: 90.0625px;\">GSLV-F06<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">GSAT-4<\/td>\r\n<td style=\"width: 74.0625px;\">Apr 15, 2010<\/td>\r\n<td style=\"width: 86.0625px;\">2220 Kg<\/td>\r\n<td style=\"width: 90.0625px;\">GSLV-D3<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">INSAT-4CR<\/td>\r\n<td style=\"width: 74.0625px;\">Sep 02, 2007<\/td>\r\n<td style=\"width: 86.0625px;\">2,130 kg<\/td>\r\n<td style=\"width: 90.0625px;\">GSLV-F04<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">INSAT-4B<\/td>\r\n<td style=\"width: 74.0625px;\">Mar 12, 2007<\/td>\r\n<td style=\"width: 86.0625px;\">3025 Kg<\/td>\r\n<td style=\"width: 90.0625px;\">Ariane5<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">INSAT-4C<\/td>\r\n<td style=\"width: 74.0625px;\">Jul 10, 2006<\/td>\r\n<td style=\"width: 86.0625px;\"><\/td>\r\n<td style=\"width: 90.0625px;\">GSLV-F02<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">INSAT-4A<\/td>\r\n<td style=\"width: 74.0625px;\">Dec 22, 2005<\/td>\r\n<td style=\"width: 86.0625px;\">3081 Kg<\/td>\r\n<td style=\"width: 90.0625px;\">Ariane5-V169<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">GSAT-17<\/td>\r\n<td style=\"width: 74.0625px;\">Jun 29, 2017<\/td>\r\n<td style=\"width: 86.0625px;\">3477 kg<\/td>\r\n<td style=\"width: 90.0625px;\">Ariane-5 VA-238<\/td>\r\n<td style=\"width: 57.0625px;\">GTO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">GSAT-19<\/td>\r\n<td style=\"width: 74.0625px;\">Jun 05, 2017<\/td>\r\n<td style=\"width: 86.0625px;\">3136 Kg<\/td>\r\n<td style=\"width: 90.0625px;\">GSLV Mk III-D1<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">GSAT-9<\/td>\r\n<td style=\"width: 74.0625px;\">May 05, 2017<\/td>\r\n<td style=\"width: 86.0625px;\">2230 kg<\/td>\r\n<td style=\"width: 90.0625px;\">GSLV-F09<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">GSAT-18<\/td>\r\n<td style=\"width: 74.0625px;\">Oct 06, 2016<\/td>\r\n<td style=\"width: 86.0625px;\">3404 kg<\/td>\r\n<td style=\"width: 90.0625px;\">Ariane-5 VA-231<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">GSAT-15<\/td>\r\n<td style=\"width: 74.0625px;\">Nov 11, 2015<\/td>\r\n<td style=\"width: 86.0625px;\">3164 kg<\/td>\r\n<td style=\"width: 90.0625px;\">Ariane-5 VA-227<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication, Navigation<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">GSAT-6<\/td>\r\n<td style=\"width: 74.0625px;\">Aug 27, 2015<\/td>\r\n<td style=\"width: 86.0625px;\">2117 kg<\/td>\r\n<td style=\"width: 90.0625px;\">GSLV-D6<\/td>\r\n<td style=\"width: 57.0625px;\">GTO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">GSAT-16<\/td>\r\n<td style=\"width: 74.0625px;\">Dec 07, 2014<\/td>\r\n<td style=\"width: 86.0625px;\">3181.6 kg<\/td>\r\n<td style=\"width: 90.0625px;\">Ariane-5 VA-221<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">GSAT-14<\/td>\r\n<td style=\"width: 74.0625px;\">Jan 05, 2014<\/td>\r\n<td style=\"width: 86.0625px;\">1982 kg<\/td>\r\n<td style=\"width: 90.0625px;\">GSLV-D5<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<tr>\r\n<td style=\"width: 87.0625px;\">GSAT-7<\/td>\r\n<td style=\"width: 74.0625px;\">Aug 30, 2013<\/td>\r\n<td style=\"width: 86.0625px;\">2650 kg<\/td>\r\n<td style=\"width: 90.0625px;\">Ariane-5 VA-215<\/td>\r\n<td style=\"width: 57.0625px;\">GSO<\/td>\r\n<td style=\"width: 116.063px;\">Communication<\/td>\r\n<\/tr>\r\n<\/tbody>\r\n<\/table>\r\n&nbsp;\r\n<p style=\"text-align: justify;\">The INSAT-1 series satellites were multipurpose satellites made by Ford Aerospace US based on Indian design and services requirements. These satellite were launched by foreign launcher Ariane and Delta. INSAT-2 series and onwards all satellites were indigenous satellite made by ISRO. After the INSAT series, the GSAT series started. Several.Satellite of GSAT and INSAT-2,-4,-3 series whose weight are less than 3000 Kg have been launched from Indian Launch Pad at SHAR by PSLV or GSLV launch vehicles. The earlier satellites were designed for 10 year\u2019s operational life.\u00a0 Nowadays satellites in Geostationary orbit have more than 15 year\u2019s designed life.<\/p>\r\n&nbsp;\r\n<p class=\"hanging-indent\"><strong> Operational Indian Satellites in Space<\/strong><\/p>\r\n\r\n<ul>\r\n \t<li style=\"text-align: justify;\">Currently operational 42 satellites in orbit<\/li>\r\n \t<li style=\"text-align: justify;\">18 Earth observation (including here are meteorological)<\/li>\r\n \t<li style=\"text-align: justify;\">15 communication<\/li>\r\n \t<li style=\"text-align: justify;\">7 navigational and<\/li>\r\n \t<li style=\"text-align: justify;\">2 Space Science satellites<\/li>\r\n \t<li style=\"text-align: justify;\">26 satellites are currently in various stages of realization<\/li>\r\n<\/ul>\r\n<strong>Major Application Areas<\/strong>\r\n<ul>\r\n \t<li style=\"text-align: justify;\">Resources monitoring, infrastructure planning, enabling weather forecasting, disaster management support, location based services, host of societal applications, including the demands of satellite communication.<\/li>\r\n \t<li style=\"text-align: justify;\">Agriculture, forestry &amp; environment, water resources, urban &amp; rural planning, asset mapping, mineral prospecting, ocean resources, meteorology, satellite communication, location based services, tele-education, tele-medicine and disaster management support.<\/li>\r\n<\/ul>\r\n<strong>Basics of Geo-stationary Satellites<\/strong>\r\n\r\n&nbsp;\r\n<p style=\"text-align: justify;\">Satellites orbit around the earth in circular or elliptical orbits. They are at same distance to the earth\u2019s surface as per the given law:<\/p>\r\n\r\n<ul>\r\n \t<li style=\"text-align: justify;\">The gravitational force of the earth given as Fg = <em>m.g<\/em>.(<em>R\/r<\/em>)2<\/li>\r\n \t<li style=\"text-align: justify;\">The centrifugal force trying to pull the satellite away given as <em>Fc <\/em>= <em>m\u00b7r\u00b7<\/em>\u03c92.<\/li>\r\n<\/ul>\r\n<p style=\"text-align: justify;\">Where m is the mass of the satellite; <em>R <\/em>is the radius of earth with <em>R <\/em>= 6,370 km;\u00a0\u00a0\u00a0\u00a0 <em>r <\/em>is the distance of the satellite to the centre of the earth; <em>g <\/em>is the acceleration of gravity \u00a0with <em>g<\/em><\/p>\r\n<p style=\"text-align: justify;\">= 9.81 m\/s2; \u03c9 is the angular velocity with \u03c9 = 2\u00b7\u03c0\u00b7<em>f<\/em>, <em>f <\/em>is the frequency of the rotation. To keep the satellite in a stable circular orbit, the following equation must hold:<\/p>\r\n<em>Fg <\/em>= <em>Fc<\/em>\r\n<ul>\r\n \t<li style=\"text-align: justify;\">Attractive force Fg = m g (R\/r)\u00b2<\/li>\r\n \t<li style=\"text-align: justify;\">Centrifugal force Fc = m v\u00b2\/r | since mgR\u00b2\/r\u00b2 = mv\u00b2\/r For Stable orbit<\/li>\r\n<\/ul>\r\n<p style=\"text-align: justify;\">Fg = Fc<\/p>\r\n<p style=\"text-align: justify;\">Or r = g R\u00b2\/v\u00b2<\/p>\r\n<p style=\"text-align: justify;\">Solving the equation for the distance r of the satellite to the center of the earth results in the following equation:<\/p>\r\n<p style=\"text-align: justify;\">The distance <em>r <\/em>= (g\u00b7<em>R<\/em>2\/(2\u00b7\u03c0\u00b7<em>f<\/em>)2)1\/3<\/p>\r\n<p style=\"text-align: justify;\">From the above equation it can be concluded that the <strong><em>distance of a satellite to the earth\u2019s surface depends on its rotation frequency<\/em><\/strong>. Figure 6.shows this dependency in addition to the relative velocity of a satellite. The interesting point in the diagram is when the satellite period equals 24 hours. This is exactly the case for a <strong>distance of 35,786 km<\/strong>. Having an <strong>orbiting time of 24 hours implies a geostationary satellite <\/strong>if it is additionally placed above the equator.<\/p>\r\n&nbsp;\r\n<p class=\"hanging-indent\" style=\"text-align: center;\"><strong>Fig. 6 Dependency of satellite period and distance to earth<\/strong><\/p>\r\n&nbsp;\r\n\r\n<img class=\"aligncenter size-full wp-image-363\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic6.png\" alt=\"\" width=\"697\" height=\"398\" \/>\r\n<p style=\"text-align: center;\"><strong>Figure 6 :<\/strong><\/p>\r\n&nbsp;\r\n<p class=\"hanging-indent\"><strong>Satellite Inclination angle<\/strong><\/p>\r\n&nbsp;\r\n<p style=\"text-align: justify;\"><strong>Inclination angle (<\/strong><em>\u03b4): T<\/em>he angle between the equatorial plane and the plane described by the satellite orbit(Figure 7). <strong>An inclination angle of 0 degrees means that the satellite is exactly above the equator. If the satellite does not have a circular orbit, the closest point to the earth is called the perigee.<\/strong><\/p>\r\n&nbsp;\r\n\r\n<img class=\"aligncenter size-full wp-image-364\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic7.png\" alt=\"\" width=\"701\" height=\"405\" \/>\r\n<p style=\"text-align: center;\"><strong>Figure 7 : Inclination angle of satellite<\/strong><\/p>\r\n&nbsp;\r\n<p class=\"hanging-indent\"><strong>Satellite Elevation Angle<\/strong><\/p>\r\n&nbsp;\r\n<p style=\"text-align: justify;\">E<strong>l<\/strong><strong>evation angle <\/strong><em>\u03b5 : T<\/em>he angle between the center of the satellite beam and the plane tangential to the earth\u2019s surface.<\/p>\r\n<p style=\"text-align: justify;\">F<strong>ootprint: T<\/strong>he area on earth where the signals of the satellite can be received.<\/p>\r\n&nbsp;\r\n\r\n<img class=\"aligncenter size-full wp-image-365\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic8.png\" alt=\"\" width=\"733\" height=\"441\" \/>\r\n<p style=\"text-align: center;\"><strong>Figure 8 : Satellite Elevation Angle<\/strong><\/p>\r\n&nbsp;\r\n<p class=\"hanging-indent\"><strong>Satellite Orbits<\/strong><\/p>\r\n&nbsp;\r\n<p style=\"text-align: justify;\">Four different types of orbits can be identified as shown in Figure 10:<\/p>\r\n\r\n<ul>\r\n \t<li style=\"text-align: justify;\">Geostationary (or geosynchronous) earth orbit (GEO): GEO satellites have a distance of almost 36,000 km to the earth. TV and radio broadcast weather satellites and satellites operating as backbones for the telephone network are some of the examples.<\/li>\r\n<\/ul>\r\n<img class=\"aligncenter wp-image-366 size-medium\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic9-300x194.png\" alt=\"\" width=\"300\" height=\"194\" \/>\r\n<p style=\"text-align: center;\"><strong>Figure 9 : Different types of satellite orbits<\/strong><\/p>\r\n\r\n<ul>\r\n \t<li style=\"text-align: justify;\"><strong>Medium earth orbit (MEO): <\/strong>MEOs operate at a distance of about 5,000\u201312,000 km some upcoming systems ICO are example of this type of orbit.<\/li>\r\n \t<li style=\"text-align: justify;\"><strong style=\"text-align: initial; font-size: 1em;\">Low earth orbit (LEO): <\/strong><span style=\"text-align: initial; font-size: 1em;\">Initially LEO satellites were mainly used for espionage, nowadays many satellites use this class with altitudes of 500\u20131,500 km. Globalstar, Iradium are examples of LEO satellites.<\/span><\/li>\r\n<\/ul>\r\n<img class=\"aligncenter size-full wp-image-367\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic10.png\" alt=\"\" width=\"497\" height=\"521\" \/>\r\n<p style=\"text-align: center;\"><strong>Figure 10 : One way satellite Delay<\/strong><\/p>\r\n&nbsp;\r\n<ul>\r\n \t<li style=\"text-align: justify;\"><strong>Highly elliptical orbit (HEO): A<\/strong>ll the satellites with noncircular orbits belong to this class. Currently, only a few commercial communication systems using satellites with elliptical orbits are planned. These systems have their perigee over large cities to improve communication quality.<\/li>\r\n<\/ul>\r\n<img class=\"aligncenter size-full wp-image-368\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic11.png\" alt=\"\" width=\"701\" height=\"398\" \/>\r\n<p style=\"text-align: center;\"><strong>Figure 11 : Frequency Bands, Spectrum Characteristics<\/strong><\/p>\r\n&nbsp;\r\n<p class=\"hanging-indent\"><strong>Frequency Bands<\/strong><\/p>\r\n&nbsp;\r\n\r\n<img class=\"aligncenter size-full wp-image-369\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic12.png\" alt=\"\" width=\"1363\" height=\"133\" \/>\r\n<p style=\"text-align: center;\"><strong>Figure 12 :<\/strong><\/p>\r\n&nbsp;\r\n<p class=\"hanging-indent\" style=\"text-align: justify;\">There are specific frequency ranges used by commercial satellites.<\/p>\r\n\r\n<ul>\r\n \t<li style=\"text-align: justify;\">L-band (Mobile Satellite Services) \u00a01.0 \u2013 2.0 GHz<\/li>\r\n \t<li style=\"text-align: justify;\">S-band (MSS, DARS \u2013 XM, Sirius)\u00a0\u00a0 1.55 \u2013 3.9 GHz<\/li>\r\n \t<li style=\"text-align: justify;\">C-band (FSS, VSAT)\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0 3.7 \u2013 6.2 GHz<\/li>\r\n \t<li style=\"text-align: justify;\">X-Band (Military\/Satellite Imagery) \u00a08.0 \u2013 12.0 GHz<\/li>\r\n \t<li style=\"text-align: justify;\">Ku-band (FSS, DBS, VSAT)\u00a0\u00a0\u00a0\u00a0 11.7\u201314.5 GHz<\/li>\r\n \t<li style=\"text-align: justify;\">Ka-band (FSS \u201cbroadband\u201d &amp; inter-satellite links) 17.7 - 21.2GHz &amp; 27.5 \u2013 31GHz.\u00a0 Indian Communication satellites are being done are in all several frequency band like L, S, Lower \u00a0extended \u00a0C \u00a0(Cext-lower), Normal \u00a0C \u00a0(Cn), \u00a0Extended \u00a0Upper \u00a0C( \u00a0Cext-upper), \u00a0Ku, \u00a0Ka Frequency bands. The Up-Link frequency and Down-Link Frequency has been indicated in Table-2,<\/li>\r\n<\/ul>\r\n<p style=\"text-align: center;\"><strong>Table 2 : Frequency Bands - Indian Communication Satellites<\/strong><\/p>\r\n&nbsp;\r\n\r\n<img class=\"aligncenter size-full wp-image-370\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic13.png\" alt=\"\" width=\"987\" height=\"387\" \/>\r\n\r\n&nbsp;\r\n<p class=\"hanging-indent\"><strong style=\"text-align: initial; text-indent: 1em; font-size: 1em;\">Conclusions<\/strong><\/p>\r\n&nbsp;\r\n<p style=\"text-align: justify;\">The communication satellites are essential elements in Mobile Communications. All orbital configurations LEO,\u00a0 MEO and GEO are required for\u00a0 MSS purpose. India has several communication satellite in GEO with various frequency band. The space and Ground segments together are helpful in mobile services in global network. In past 50 years the tremendous growth took place in the satellites field and their service which has potentially increased the data rate as well as band width. Advance multi-beam satellites, along with free space RF and Optical link will govern the future applications in mobile services for seamless connectivity.<\/p>\r\n<table>\r\n<tbody>\r\n<tr>\r\n<td><strong>you can view video on Mobile communications Satellite systems (Part-1)<\/strong><\/td>\r\n<td><a href=\"https:\/\/youtu.be\/uIzBLF30nLI\" target=\"_blank\" rel=\"noopener\"><img class=\"alignnone wp-image-120\" src=\"http:\/\/epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/2018\/11\/download.png\" alt=\"\" width=\"36\" height=\"36\" \/><\/a><\/td>\r\n<\/tr>\r\n<\/tbody>\r\n<\/table>\r\n\r\n<p class=\"hanging-indent\"><strong>Suggested Reading:<\/strong><\/p>\r\n\r\n<ol>\r\n \t<li style=\"text-align: justify;\">Mobile Communication 2nd edition by Jochen Schiller, Pearson education<\/li>\r\n \t<li style=\"text-align: justify;\">Mobile Computing by Asoke Talukder, Roopa Yavagal (Tata McGraw Hill)<\/li>\r\n \t<li style=\"text-align: justify;\">\"Wireless communication and networking\" by William Stallings<\/li>\r\n \t<li style=\"text-align: justify;\">Mobile Cellular Telecommunications \u2014 W.C.Y. Lee, Mc Graw Hill<\/li>\r\n \t<li style=\"text-align: justify;\">Wireless Communications \u2013 Theodore. S. Rapport, Pearson Education<\/li>\r\n \t<li style=\"text-align: justify;\">Reza B'Far (Ed), \"Mobile Computing Principles\", Cambridge University Press.<\/li>\r\n<\/ol>","rendered":"<div><span style=\"float: right;\"><a href=\"https:\/\/youtu.be\/uIzBLF30nLI\" target=\"_blank\" rel=\"noopener\"><img decoding=\"async\" src=\"http:\/\/epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/2018\/11\/download.png\" alt=\"epgp books\" width=\"75px\" height=\"75px;\" \/><\/a><br \/>\n<\/span><\/div>\n<p><strong>Learning Objectives<\/strong><\/p>\n<ul>\n<li>Communication satellite Segments<\/li>\n<li>History Satellite communication<\/li>\n<li>Classical Satellite Systems<\/li>\n<li>Applications<\/li>\n<li>Indian Communication Satellites and Critical Services<\/li>\n<li>Basics of Geo-stationary Satellites<\/li>\n<li>satellite Inclination angle<\/li>\n<li>Satellite Elevation Angle<\/li>\n<li>Propagation Loss<\/li>\n<li>Satellite Orbits<\/li>\n<li>GEO<\/li>\n<li>LEO<\/li>\n<li>MEO<\/li>\n<li>Frequency Bands, Spectrum<\/li>\n<\/ul>\n<p class=\"hanging-indent\"><strong>Introduction<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\">Satellite communication supports the mobile communications. Satellites offer global coverage without wiring costs for base stations and are almost independent of varying population densities.<\/p>\n<p>&nbsp;<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"aligncenter size-full wp-image-358\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic1.png\" alt=\"\" width=\"253\" height=\"189\" srcset=\"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic1.png 253w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic1-65x49.png 65w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic1-225x168.png 225w\" sizes=\"auto, (max-width: 253px) 100vw, 253px\" \/><\/p>\n<p style=\"text-align: center;\"><strong>Figure 1<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p class=\"hanging-indent\"><strong>Satellite Communication can be broadly divided in three segments<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"aligncenter size-full wp-image-359\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic2.png\" alt=\"\" width=\"1014\" height=\"357\" srcset=\"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic2.png 1014w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic2-300x106.png 300w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic2-768x270.png 768w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic2-65x23.png 65w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic2-225x79.png 225w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic2-350x123.png 350w\" sizes=\"auto, (max-width: 1014px) 100vw, 1014px\" \/><\/p>\n<p style=\"text-align: center;\"><strong>Figure 2 : Space Communication Segments<\/strong><\/p>\n<ol>\n<li style=\"text-align: justify;\">Space Segments: consists of mainly Communication satellites in various orbits GEO, LEO, MEO and HEO depending upon the application needs to the users<\/li>\n<li style=\"text-align: justify;\">Ground Segments: consists of mainly Hub or Gateway Earth Station user terminal.<\/li>\n<li style=\"text-align: justify;\">Communication Channel Communication is established by Up link and Down link frequency in UHF, L band, S-band, Normal C-band, Extended C-band, Ku-band, X-band, Ka-band, Q-band, V-band, W-band, Optical-bands etc. depending on the user application, approval by ITU, band width, Geographical location, data rate, data volume and traffic density requirements.<\/li>\n<\/ol>\n<p style=\"text-align: justify;\">The high speed of satellites with a low altitude raises new problems for routing, localization of mobile users, and handover of communication links.<\/p>\n<p>&nbsp;<\/p>\n<div>\n<p><strong>History Satellite communication<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\">Satellite communication began after the Second World War. In 1945, Arthur C. Clarke published his essay on \u2018Extra Terrestrial Relays\u2019. But it was not until 1957, in the middle of the cold war, that the\u00a0 sudden launching of the first satellite SPUTNIK by the Soviet Union shocked the Western world. SPUTNIK is not at all comparable to a satellite today; it was basically a small sender transmitting a periodic \u2018beep\u2019.<\/p>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\">Today, geostationary satellites are the backbone of news broadcasting in the sky. Their great advantage is their fixed position in the sky. Their rotation is synchronous to the rotation of the earth, so they appear to be pinned to a certain location.<\/p>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\"><span style=\"font-size: 1em;\">The first commercial geostationary communication satellite INTELSAT 1 (also known as \u2018Early Bird\u2019) went into operation in 1965. It was in service for one-and-a-half years, weighed 68 kg and offered 240 duplex telephone channels or, alternatively, a single TV channel. INTELSAT 2 followed in 1967, INTELSAT- 3 in 1969 already offered 1,200 telephone channels. While communication on land always provides the alternative of using wires, this is not the case for ships at sea. Three MARISAT satellites went into operation in 1976 which offered worldwide maritime communication. However, Sender and receiver still had to be installed on the ships with large antennas (1.2 m antenna, 40 W transmit power). The first mobile satellite telephone system, INMARSAT-A, was introduced in 1982. Six years later, INMARSAT-C became the first satellite system to offer mobile phone and data services. (Data rates of about 600 bit\/s, interfaces to the X.25 packet data network exist.) In 1993, satellite telephone systems finally became fully digital with INMARSAT-M.<\/span><\/p>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\"><span style=\"font-size: 1em;\">Nineteen ninety-eight marked the beginning of a new age of satellite data communication with <\/span><span style=\"font-size: 1em;\">the introduction of global satellite systems for small mobile phones, such as, e.g., Iridium and Global star. There are more than 2000 geostationary satellites in commercial use which shows the impressive growth of satellite communication over the last 50 years.<\/span><\/p>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\"><span style=\"font-size: 1em;\">The Indian Space Program was started by 1969, by Great Visionary Dr.Vikram Sarabhai. The first Indian Satellite INSAT-1A was launched in 1981. Currently INSAT and GSAT series 42 satellites are operational in orbit.<\/span><\/p>\n<\/div>\n<p class=\"hanging-indent\" style=\"text-align: justify;\"><strong>Classical Satellite Systems<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\">Earlier satellites were simple transponders; today\u2019s satellites rather resemble flying routers. Transponders basically receive a signal on one frequency, amplify the signal and transmit it on another frequency. While in the beginning only analog amplification was possible, the use of digital signals also allows for signal regeneration. The satellite decodes the signal into a bit stream, and codes it again into a signal. The advantage of digital regeneration compared to pure analog amplification is the higher quality of the received signal on the earth. Today\u2019s communication satellites provide many functions of higher communication layers, e.g., inter- satellite routing, error correction etc.<\/p>\n<p>&nbsp;<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"aligncenter size-full wp-image-360\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic3.png\" alt=\"\" width=\"573\" height=\"370\" srcset=\"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic3.png 573w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic3-300x194.png 300w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic3-65x42.png 65w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic3-225x145.png 225w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic3-350x226.png 350w\" sizes=\"auto, (max-width: 573px) 100vw, 573px\" \/><\/p>\n<p style=\"text-align: center;\"><strong>Figure 3 : Classical Satellite Systems<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\">Figure 3 shows a classical scenario for satellite systems supporting global mobile communication. Depending on its type, each satellite can cover a certain area on the earth with its beam (the so-called \u2018footprint\u2019. Within the footprint, communication with the satellite is possible for mobile users via a <strong>mobile user link (MUL) <\/strong>and for the base station controlling the satellite and acting as gateway to other networks via the <strong>gateway link (GWL)<\/strong>. Satellites may be able to communicate directly with each other via <strong>i<\/strong><strong>ntersatellite links (ISL)<\/strong>.<\/p>\n<p>&nbsp;<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"aligncenter wp-image-361 size-full\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic4.png\" alt=\"\" width=\"892\" height=\"373\" srcset=\"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic4.png 892w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic4-300x125.png 300w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic4-768x321.png 768w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic4-65x27.png 65w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic4-225x94.png 225w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic4-350x146.png 350w\" sizes=\"auto, (max-width: 892px) 100vw, 892px\" \/><\/p>\n<p style=\"text-align: center;\"><strong>Figure 4 : Communication Satellites &#8211; Intersatellite Link (ISL).<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\"><span style=\"text-align: justify; font-size: 1em;\">This facilitates direct communication between users within different footprints without using base stations or other networks on earth. Saving extra links from satellite to earth can reduce latency for data packets and voice data. Some satellites have special antennas to create smaller cells using spot beams (e.g., 163 spot beams per satellite in the ICO system (ICO, 2002)). The required terrestrial service infrastructure for satellite control and the control links between. Satellite systems will continue to be, a valuable addition to the many networks already in existence on earth. Users might communicate using ISDN or other PSTN, even cellular networks\u00a0<\/span><span style=\"text-align: initial; font-size: 1em;\">such as\u00a0 GSM and UMTS. Many\u00a0 gateways provide seamless communication between these different networks. A real challenge, for example, is the smooth, seamless handover between a cellular network and a satellite system (vertical handover) as it is already well known from within cellular networks (horizontal handover). Users should not notice the switching from, e.g., GSM, to a satellite network during conversation.<\/span><\/p>\n<div>\n<ul>\n<li style=\"text-align: justify;\"><strong>Applications \u00a0<\/strong>Traditionally, satellites have been used in the following areas:<\/li>\n<li style=\"text-align: justify;\"><strong>Weather forecasting: <\/strong>Satellites are used to capture picture of the earth and relay on ground station to predict the weather conditions. It is very useful to predict anomalies like Hurricane beforehand so that preventive measures can be taken,<\/li>\n<li style=\"text-align: justify;\"><strong>R<\/strong><strong>a<\/strong><strong>dio and TV broadcast satellites: <\/strong>Satellites and easy and cheap alternative to cable network for radio and television broadcasting.<\/li>\n<li style=\"text-align: justify;\"><strong>Military satellites: C<\/strong>ommunication links managed through satellite because they are safer from attack by enemies Most of the Military satellites operate on X-band.<\/li>\n<li style=\"text-align: justify;\"><strong>Satellites for navigation: <\/strong>The global positioning system (GPS) provides precise localization information with high precision of few meters. All ships and aircraft use GPS for their navigation systems. Information obtained from GPS receivers installed in vehicles is used for fleet management localization of vehicles etc. The Indian Space Research Organization (ISRO) has developed indigenous Indian Regional Navigation Satellite System called \u201cNavIC\u201d as deshi GPS with 7 GEO\/GSO satellites. It has become operational. It can replace the most popular GPS of US, Glonass of Russia, Beidou of China or Galileo of European. NavIC System can develop potential application for Road Navigation, Rail Navigation and safety, Generate warning for unmanned Level Crossing, Vessel Monitoring and Tracking for costal Surveillance, Surveying \u2013Land, Marine, Differential correction with Geodetic Receivers, Disaster management and warning, Emergency Calling, Location based services, Ionospheric monitoring and scintillation studies, Time and Frequency synchronization for Internet and Intranet application and several applications for Scientific and Research communities and Services to society.<\/li>\n<li style=\"text-align: justify;\"><strong>Global telephone backbones: <\/strong>Communication satellites are emerging as an alternative to cables for international telephone backbone .The satellites are increasingly being replaced by fiber optical cables crossing the oceans. The main reason for this is the tremendous capacity of fiber optical links (commercially some 10 Gbit\/s using wavelength division\u00a0<span style=\"text-align: initial; font-size: 1em;\">multiplexing, several Tbit\/s in labs) and, in particular, the much lower delay compared to satellites. While the signal to a geostationary satellite has to travel about 72,000 km from a sender via the satellite to the receiver, the distance is typically less than 10,000 km if a fiber-optical link crossing the Pacific or Atlantic Ocean is used. Unfortunately, the speed of light is limited, resulting in a one-way, single-hop time delay of 0.25 s for geostationary satellites. Using satellites for telephone conversation is sometimes annoying.<\/span><\/li>\n<li style=\"text-align: justify;\"><strong style=\"font-size: 1em;\">C<\/strong><strong style=\"font-size: 1em;\">onnections for remote or developing areas: <\/strong><span style=\"font-size: 1em;\">Satellites offer a simple and quick connection to global networks to the places which are inaccessible due to their geographical location.<\/span><\/li>\n<li style=\"text-align: justify;\"><strong style=\"text-align: initial; font-size: 1em;\">Global mobile communication: <\/strong><span style=\"text-align: initial; font-size: 1em;\">Most recent advantage of satellites is mobile data communication. Geostationary satellites are not ideal for this because of high latency rate therefore; there is need of satellites using using lower orbits. Use of satellites for mobile communication is not as a replacer but as an extension to existing systems. They have an edge over existing cellular systems such as AMPS and GSM because of world wide coverage. For the UMTS system frequency bands directly adjacent to the terrestrial bands have been allocated for the satellite segment (S-Band: 1980\u20132010 MHz uplink, 2170\u20132200 MHz downlink).<\/span><\/li>\n<\/ul>\n<\/div>\n<p style=\"text-align: justify;\"><strong>INDIAN Critical Services through Indigenous Communication Satellites<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"aligncenter size-full wp-image-362\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic5.png\" alt=\"\" width=\"1008\" height=\"846\" srcset=\"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic5.png 1008w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic5-300x252.png 300w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic5-768x645.png 768w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic5-65x55.png 65w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic5-225x189.png 225w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic5-350x294.png 350w\" sizes=\"auto, (max-width: 1008px) 100vw, 1008px\" \/><\/p>\n<p style=\"text-align: center;\"><strong>Figure 5 : Indian Critical Services via Communication Satellites.<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\">India\u2019s INSAT and GSAT series of communication satellites are offering UHF, S-band Normal C band, Cext Cband, Ku-Band and Ka band multi band multipurpose Transponders for Telecommunication, Broadcasting, DTH, VSAT\/Business Communication Societal Development, Dedicated satellite for Tele-education, e-learning, Telemedicine, METSAT and Disaster services, mobile services, advance communication services for internet, high throughput satellite for more cannels and higher data rate and many more services for country\u2019s development program.<\/p>\n<p>&nbsp;<\/p>\n<p class=\"hanging-indent\"><strong>Indian Communication Satellites<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p class=\"hanging-indent\"><strong>Table 1 :<\/strong><\/p>\n<table class=\"lines\" style=\"height: 1619px; width: 600px; margin: auto;\">\n<tbody>\n<tr>\n<td style=\"width: 87.0625px;\">SATELLITE<\/td>\n<td style=\"width: 74.0625px;\">Launch Date<\/td>\n<td style=\"width: 86.0625px;\">Launch Mass<\/td>\n<td style=\"width: 90.0625px;\">Launch Vehicle<\/td>\n<td style=\"width: 57.0625px;\">Orbit<\/td>\n<td style=\"width: 116.063px;\">Application<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">INSAT-3B<\/td>\n<td style=\"width: 74.0625px;\">Mar 22, 2000<\/td>\n<td style=\"width: 86.0625px;\">2,070 Kg<\/td>\n<td style=\"width: 90.0625px;\">Ariane-5G<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">INSAT-2E<\/td>\n<td style=\"width: 74.0625px;\">Apr 03, 1999<\/td>\n<td style=\"width: 86.0625px;\">2,550 Kg<\/td>\n<td style=\"width: 90.0625px;\">Ariane-42P H10-3<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">INSAT-2D<\/td>\n<td style=\"width: 74.0625px;\">Jun 04, 1997<\/td>\n<td style=\"width: 86.0625px;\">2079 Kg<\/td>\n<td style=\"width: 90.0625px;\">Ariane-44L H10-3<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">INSAT-2C<\/td>\n<td style=\"width: 74.0625px;\">Dec 07, 1995<\/td>\n<td style=\"width: 86.0625px;\">2106 Kg<\/td>\n<td style=\"width: 90.0625px;\">Ariane-44L H10-3<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">INSAT-2B<\/td>\n<td style=\"width: 74.0625px;\">Jul 23, 1993<\/td>\n<td style=\"width: 86.0625px;\">1906 kg<\/td>\n<td style=\"width: 90.0625px;\">Ariane-44L H10+<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">INSAT-2A<\/td>\n<td style=\"width: 74.0625px;\">Jul 10, 1992<\/td>\n<td style=\"width: 86.0625px;\">1906 kg<\/td>\n<td style=\"width: 90.0625px;\">Ariane-44L H10<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">INSAT-1D<\/td>\n<td style=\"width: 74.0625px;\">Jun 12, 1990<\/td>\n<td style=\"width: 86.0625px;\"><\/td>\n<td style=\"width: 90.0625px;\">Delta 4925<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">INSAT-1C<\/td>\n<td style=\"width: 74.0625px;\">Jul 22, 1988<\/td>\n<td style=\"width: 86.0625px;\"><\/td>\n<td style=\"width: 90.0625px;\">Ariane-3<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">INSAT-1B<\/td>\n<td style=\"width: 74.0625px;\">Aug 30, 1983<\/td>\n<td style=\"width: 86.0625px;\"><\/td>\n<td style=\"width: 90.0625px;\">Shuttle [PAM-D]<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">INSAT-1A<\/td>\n<td style=\"width: 74.0625px;\">Apr 10, 1982<\/td>\n<td style=\"width: 86.0625px;\"><\/td>\n<td style=\"width: 90.0625px;\">Delta<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">HAMSAT<\/td>\n<td style=\"width: 74.0625px;\">May 05, 2005<\/td>\n<td style=\"width: 86.0625px;\"><\/td>\n<td style=\"width: 90.0625px;\">PSLV-C6<\/td>\n<td style=\"width: 57.0625px;\">SSPO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">EDUSAT<\/td>\n<td style=\"width: 74.0625px;\">Sep 20, 2004<\/td>\n<td style=\"width: 86.0625px;\">1950.5 kg<\/td>\n<td style=\"width: 90.0625px;\">GSLV-F01<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">INSAT-3E<\/td>\n<td style=\"width: 74.0625px;\">Sep 28, 2003<\/td>\n<td style=\"width: 86.0625px;\">2,775 Kg<\/td>\n<td style=\"width: 90.0625px;\">Ariane5-V162<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">GSAT-2<\/td>\n<td style=\"width: 74.0625px;\">May 08, 2003<\/td>\n<td style=\"width: 86.0625px;\">1800 Kg<\/td>\n<td style=\"width: 90.0625px;\">GSLV-D2<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">INSAT-3A<\/td>\n<td style=\"width: 74.0625px;\">Apr 10, 2003<\/td>\n<td style=\"width: 86.0625px;\">2,950 Kg<\/td>\n<td style=\"width: 90.0625px;\">Ariane5-V160<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Climate &amp; Environm., Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">KALPANA-1<\/td>\n<td style=\"width: 74.0625px;\">Sep 12, 2002<\/td>\n<td style=\"width: 86.0625px;\">1060 Kg<\/td>\n<td style=\"width: 90.0625px;\">PSLV-C4<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Climate &amp; Environm. Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">INSAT-3C<\/td>\n<td style=\"width: 74.0625px;\">Jan 24, 2002<\/td>\n<td style=\"width: 86.0625px;\">2,650 Kg<\/td>\n<td style=\"width: 90.0625px;\">Ariane5-V147<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Climate &amp; Environ., Commun<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">GSAT-1<\/td>\n<td style=\"width: 74.0625px;\">Apr 18, 2001<\/td>\n<td style=\"width: 86.0625px;\">1530 Kg<\/td>\n<td style=\"width: 90.0625px;\">GSLV-D1<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">HAMSAT<\/td>\n<td style=\"width: 74.0625px;\">May 05, 2005<\/td>\n<td style=\"width: 86.0625px;\"><\/td>\n<td style=\"width: 90.0625px;\">PSLV-C6<\/td>\n<td style=\"width: 57.0625px;\">SSPO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">GSAT-12<\/td>\n<td style=\"width: 74.0625px;\">Jul 15, 2011<\/td>\n<td style=\"width: 86.0625px;\">1410 kg<\/td>\n<td style=\"width: 90.0625px;\">PSLV-C17<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">GSAT-8<\/td>\n<td style=\"width: 74.0625px;\">May 21, 2011<\/td>\n<td style=\"width: 86.0625px;\">3093 kg<\/td>\n<td style=\"width: 90.0625px;\">Ariane-5 VA-202<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication, Navigation<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">GSAT-5P<\/td>\n<td style=\"width: 74.0625px;\">Dec 25, 2010<\/td>\n<td style=\"width: 86.0625px;\">2310 kg<\/td>\n<td style=\"width: 90.0625px;\">GSLV-F06<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">GSAT-4<\/td>\n<td style=\"width: 74.0625px;\">Apr 15, 2010<\/td>\n<td style=\"width: 86.0625px;\">2220 Kg<\/td>\n<td style=\"width: 90.0625px;\">GSLV-D3<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">INSAT-4CR<\/td>\n<td style=\"width: 74.0625px;\">Sep 02, 2007<\/td>\n<td style=\"width: 86.0625px;\">2,130 kg<\/td>\n<td style=\"width: 90.0625px;\">GSLV-F04<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">INSAT-4B<\/td>\n<td style=\"width: 74.0625px;\">Mar 12, 2007<\/td>\n<td style=\"width: 86.0625px;\">3025 Kg<\/td>\n<td style=\"width: 90.0625px;\">Ariane5<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">INSAT-4C<\/td>\n<td style=\"width: 74.0625px;\">Jul 10, 2006<\/td>\n<td style=\"width: 86.0625px;\"><\/td>\n<td style=\"width: 90.0625px;\">GSLV-F02<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">INSAT-4A<\/td>\n<td style=\"width: 74.0625px;\">Dec 22, 2005<\/td>\n<td style=\"width: 86.0625px;\">3081 Kg<\/td>\n<td style=\"width: 90.0625px;\">Ariane5-V169<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">GSAT-17<\/td>\n<td style=\"width: 74.0625px;\">Jun 29, 2017<\/td>\n<td style=\"width: 86.0625px;\">3477 kg<\/td>\n<td style=\"width: 90.0625px;\">Ariane-5 VA-238<\/td>\n<td style=\"width: 57.0625px;\">GTO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">GSAT-19<\/td>\n<td style=\"width: 74.0625px;\">Jun 05, 2017<\/td>\n<td style=\"width: 86.0625px;\">3136 Kg<\/td>\n<td style=\"width: 90.0625px;\">GSLV Mk III-D1<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">GSAT-9<\/td>\n<td style=\"width: 74.0625px;\">May 05, 2017<\/td>\n<td style=\"width: 86.0625px;\">2230 kg<\/td>\n<td style=\"width: 90.0625px;\">GSLV-F09<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">GSAT-18<\/td>\n<td style=\"width: 74.0625px;\">Oct 06, 2016<\/td>\n<td style=\"width: 86.0625px;\">3404 kg<\/td>\n<td style=\"width: 90.0625px;\">Ariane-5 VA-231<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">GSAT-15<\/td>\n<td style=\"width: 74.0625px;\">Nov 11, 2015<\/td>\n<td style=\"width: 86.0625px;\">3164 kg<\/td>\n<td style=\"width: 90.0625px;\">Ariane-5 VA-227<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication, Navigation<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">GSAT-6<\/td>\n<td style=\"width: 74.0625px;\">Aug 27, 2015<\/td>\n<td style=\"width: 86.0625px;\">2117 kg<\/td>\n<td style=\"width: 90.0625px;\">GSLV-D6<\/td>\n<td style=\"width: 57.0625px;\">GTO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">GSAT-16<\/td>\n<td style=\"width: 74.0625px;\">Dec 07, 2014<\/td>\n<td style=\"width: 86.0625px;\">3181.6 kg<\/td>\n<td style=\"width: 90.0625px;\">Ariane-5 VA-221<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">GSAT-14<\/td>\n<td style=\"width: 74.0625px;\">Jan 05, 2014<\/td>\n<td style=\"width: 86.0625px;\">1982 kg<\/td>\n<td style=\"width: 90.0625px;\">GSLV-D5<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<tr>\n<td style=\"width: 87.0625px;\">GSAT-7<\/td>\n<td style=\"width: 74.0625px;\">Aug 30, 2013<\/td>\n<td style=\"width: 86.0625px;\">2650 kg<\/td>\n<td style=\"width: 90.0625px;\">Ariane-5 VA-215<\/td>\n<td style=\"width: 57.0625px;\">GSO<\/td>\n<td style=\"width: 116.063px;\">Communication<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\">The INSAT-1 series satellites were multipurpose satellites made by Ford Aerospace US based on Indian design and services requirements. These satellite were launched by foreign launcher Ariane and Delta. INSAT-2 series and onwards all satellites were indigenous satellite made by ISRO. After the INSAT series, the GSAT series started. Several.Satellite of GSAT and INSAT-2,-4,-3 series whose weight are less than 3000 Kg have been launched from Indian Launch Pad at SHAR by PSLV or GSLV launch vehicles. The earlier satellites were designed for 10 year\u2019s operational life.\u00a0 Nowadays satellites in Geostationary orbit have more than 15 year\u2019s designed life.<\/p>\n<p>&nbsp;<\/p>\n<p class=\"hanging-indent\"><strong> Operational Indian Satellites in Space<\/strong><\/p>\n<ul>\n<li style=\"text-align: justify;\">Currently operational 42 satellites in orbit<\/li>\n<li style=\"text-align: justify;\">18 Earth observation (including here are meteorological)<\/li>\n<li style=\"text-align: justify;\">15 communication<\/li>\n<li style=\"text-align: justify;\">7 navigational and<\/li>\n<li style=\"text-align: justify;\">2 Space Science satellites<\/li>\n<li style=\"text-align: justify;\">26 satellites are currently in various stages of realization<\/li>\n<\/ul>\n<p><strong>Major Application Areas<\/strong><\/p>\n<ul>\n<li style=\"text-align: justify;\">Resources monitoring, infrastructure planning, enabling weather forecasting, disaster management support, location based services, host of societal applications, including the demands of satellite communication.<\/li>\n<li style=\"text-align: justify;\">Agriculture, forestry &amp; environment, water resources, urban &amp; rural planning, asset mapping, mineral prospecting, ocean resources, meteorology, satellite communication, location based services, tele-education, tele-medicine and disaster management support.<\/li>\n<\/ul>\n<p><strong>Basics of Geo-stationary Satellites<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\">Satellites orbit around the earth in circular or elliptical orbits. They are at same distance to the earth\u2019s surface as per the given law:<\/p>\n<ul>\n<li style=\"text-align: justify;\">The gravitational force of the earth given as Fg = <em>m.g<\/em>.(<em>R\/r<\/em>)2<\/li>\n<li style=\"text-align: justify;\">The centrifugal force trying to pull the satellite away given as <em>Fc <\/em>= <em>m\u00b7r\u00b7<\/em>\u03c92.<\/li>\n<\/ul>\n<p style=\"text-align: justify;\">Where m is the mass of the satellite; <em>R <\/em>is the radius of earth with <em>R <\/em>= 6,370 km;\u00a0\u00a0\u00a0\u00a0 <em>r <\/em>is the distance of the satellite to the centre of the earth; <em>g <\/em>is the acceleration of gravity \u00a0with <em>g<\/em><\/p>\n<p style=\"text-align: justify;\">= 9.81 m\/s2; \u03c9 is the angular velocity with \u03c9 = 2\u00b7\u03c0\u00b7<em>f<\/em>, <em>f <\/em>is the frequency of the rotation. To keep the satellite in a stable circular orbit, the following equation must hold:<\/p>\n<p><em>Fg <\/em>= <em>Fc<\/em><\/p>\n<ul>\n<li style=\"text-align: justify;\">Attractive force Fg = m g (R\/r)\u00b2<\/li>\n<li style=\"text-align: justify;\">Centrifugal force Fc = m v\u00b2\/r | since mgR\u00b2\/r\u00b2 = mv\u00b2\/r For Stable orbit<\/li>\n<\/ul>\n<p style=\"text-align: justify;\">Fg = Fc<\/p>\n<p style=\"text-align: justify;\">Or r = g R\u00b2\/v\u00b2<\/p>\n<p style=\"text-align: justify;\">Solving the equation for the distance r of the satellite to the center of the earth results in the following equation:<\/p>\n<p style=\"text-align: justify;\">The distance <em>r <\/em>= (g\u00b7<em>R<\/em>2\/(2\u00b7\u03c0\u00b7<em>f<\/em>)2)1\/3<\/p>\n<p style=\"text-align: justify;\">From the above equation it can be concluded that the <strong><em>distance of a satellite to the earth\u2019s surface depends on its rotation frequency<\/em><\/strong>. Figure 6.shows this dependency in addition to the relative velocity of a satellite. The interesting point in the diagram is when the satellite period equals 24 hours. This is exactly the case for a <strong>distance of 35,786 km<\/strong>. Having an <strong>orbiting time of 24 hours implies a geostationary satellite <\/strong>if it is additionally placed above the equator.<\/p>\n<p>&nbsp;<\/p>\n<p class=\"hanging-indent\" style=\"text-align: center;\"><strong>Fig. 6 Dependency of satellite period and distance to earth<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"aligncenter size-full wp-image-363\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic6.png\" alt=\"\" width=\"697\" height=\"398\" srcset=\"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic6.png 697w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic6-300x171.png 300w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic6-65x37.png 65w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic6-225x128.png 225w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic6-350x200.png 350w\" sizes=\"auto, (max-width: 697px) 100vw, 697px\" \/><\/p>\n<p style=\"text-align: center;\"><strong>Figure 6 :<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p class=\"hanging-indent\"><strong>Satellite Inclination angle<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\"><strong>Inclination angle (<\/strong><em>\u03b4): T<\/em>he angle between the equatorial plane and the plane described by the satellite orbit(Figure 7). <strong>An inclination angle of 0 degrees means that the satellite is exactly above the equator. If the satellite does not have a circular orbit, the closest point to the earth is called the perigee.<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"aligncenter size-full wp-image-364\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic7.png\" alt=\"\" width=\"701\" height=\"405\" srcset=\"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic7.png 701w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic7-300x173.png 300w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic7-65x38.png 65w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic7-225x130.png 225w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic7-350x202.png 350w\" sizes=\"auto, (max-width: 701px) 100vw, 701px\" \/><\/p>\n<p style=\"text-align: center;\"><strong>Figure 7 : Inclination angle of satellite<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p class=\"hanging-indent\"><strong>Satellite Elevation Angle<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\">E<strong>l<\/strong><strong>evation angle <\/strong><em>\u03b5 : T<\/em>he angle between the center of the satellite beam and the plane tangential to the earth\u2019s surface.<\/p>\n<p style=\"text-align: justify;\">F<strong>ootprint: T<\/strong>he area on earth where the signals of the satellite can be received.<\/p>\n<p>&nbsp;<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"aligncenter size-full wp-image-365\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic8.png\" alt=\"\" width=\"733\" height=\"441\" srcset=\"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic8.png 733w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic8-300x180.png 300w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic8-65x39.png 65w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic8-225x135.png 225w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic8-350x211.png 350w\" sizes=\"auto, (max-width: 733px) 100vw, 733px\" \/><\/p>\n<p style=\"text-align: center;\"><strong>Figure 8 : Satellite Elevation Angle<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p class=\"hanging-indent\"><strong>Satellite Orbits<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\">Four different types of orbits can be identified as shown in Figure 10:<\/p>\n<ul>\n<li style=\"text-align: justify;\">Geostationary (or geosynchronous) earth orbit (GEO): GEO satellites have a distance of almost 36,000 km to the earth. TV and radio broadcast weather satellites and satellites operating as backbones for the telephone network are some of the examples.<\/li>\n<\/ul>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"aligncenter wp-image-366 size-medium\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic9-300x194.png\" alt=\"\" width=\"300\" height=\"194\" srcset=\"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic9-300x194.png 300w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic9-768x497.png 768w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic9-65x42.png 65w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic9-225x146.png 225w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic9-350x227.png 350w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic9.png 851w\" sizes=\"auto, (max-width: 300px) 100vw, 300px\" \/><\/p>\n<p style=\"text-align: center;\"><strong>Figure 9 : Different types of satellite orbits<\/strong><\/p>\n<ul>\n<li style=\"text-align: justify;\"><strong>Medium earth orbit (MEO): <\/strong>MEOs operate at a distance of about 5,000\u201312,000 km some upcoming systems ICO are example of this type of orbit.<\/li>\n<li style=\"text-align: justify;\"><strong style=\"text-align: initial; font-size: 1em;\">Low earth orbit (LEO): <\/strong><span style=\"text-align: initial; font-size: 1em;\">Initially LEO satellites were mainly used for espionage, nowadays many satellites use this class with altitudes of 500\u20131,500 km. Globalstar, Iradium are examples of LEO satellites.<\/span><\/li>\n<\/ul>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"aligncenter size-full wp-image-367\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic10.png\" alt=\"\" width=\"497\" height=\"521\" srcset=\"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic10.png 497w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic10-286x300.png 286w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic10-65x68.png 65w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic10-225x236.png 225w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic10-350x367.png 350w\" sizes=\"auto, (max-width: 497px) 100vw, 497px\" \/><\/p>\n<p style=\"text-align: center;\"><strong>Figure 10 : One way satellite Delay<\/strong><\/p>\n<p>&nbsp;<\/p>\n<ul>\n<li style=\"text-align: justify;\"><strong>Highly elliptical orbit (HEO): A<\/strong>ll the satellites with noncircular orbits belong to this class. Currently, only a few commercial communication systems using satellites with elliptical orbits are planned. These systems have their perigee over large cities to improve communication quality.<\/li>\n<\/ul>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"aligncenter size-full wp-image-368\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic11.png\" alt=\"\" width=\"701\" height=\"398\" srcset=\"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic11.png 701w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic11-300x170.png 300w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic11-65x37.png 65w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic11-225x128.png 225w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic11-350x199.png 350w\" sizes=\"auto, (max-width: 701px) 100vw, 701px\" \/><\/p>\n<p style=\"text-align: center;\"><strong>Figure 11 : Frequency Bands, Spectrum Characteristics<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p class=\"hanging-indent\"><strong>Frequency Bands<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"aligncenter size-full wp-image-369\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic12.png\" alt=\"\" width=\"1363\" height=\"133\" srcset=\"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic12.png 1363w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic12-300x29.png 300w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic12-768x75.png 768w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic12-1024x100.png 1024w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic12-65x6.png 65w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic12-225x22.png 225w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic12-350x34.png 350w\" sizes=\"auto, (max-width: 1363px) 100vw, 1363px\" \/><\/p>\n<p style=\"text-align: center;\"><strong>Figure 12 :<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p class=\"hanging-indent\" style=\"text-align: justify;\">There are specific frequency ranges used by commercial satellites.<\/p>\n<ul>\n<li style=\"text-align: justify;\">L-band (Mobile Satellite Services) \u00a01.0 \u2013 2.0 GHz<\/li>\n<li style=\"text-align: justify;\">S-band (MSS, DARS \u2013 XM, Sirius)\u00a0\u00a0 1.55 \u2013 3.9 GHz<\/li>\n<li style=\"text-align: justify;\">C-band (FSS, VSAT)\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0 3.7 \u2013 6.2 GHz<\/li>\n<li style=\"text-align: justify;\">X-Band (Military\/Satellite Imagery) \u00a08.0 \u2013 12.0 GHz<\/li>\n<li style=\"text-align: justify;\">Ku-band (FSS, DBS, VSAT)\u00a0\u00a0\u00a0\u00a0 11.7\u201314.5 GHz<\/li>\n<li style=\"text-align: justify;\">Ka-band (FSS \u201cbroadband\u201d &amp; inter-satellite links) 17.7 &#8211; 21.2GHz &amp; 27.5 \u2013 31GHz.\u00a0 Indian Communication satellites are being done are in all several frequency band like L, S, Lower \u00a0extended \u00a0C \u00a0(Cext-lower), Normal \u00a0C \u00a0(Cn), \u00a0Extended \u00a0Upper \u00a0C( \u00a0Cext-upper), \u00a0Ku, \u00a0Ka Frequency bands. The Up-Link frequency and Down-Link Frequency has been indicated in Table-2,<\/li>\n<\/ul>\n<p style=\"text-align: center;\"><strong>Table 2 : Frequency Bands &#8211; Indian Communication Satellites<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"aligncenter size-full wp-image-370\" src=\"http:\/\/itp12.epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic13.png\" alt=\"\" width=\"987\" height=\"387\" srcset=\"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic13.png 987w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic13-300x118.png 300w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic13-768x301.png 768w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic13-65x25.png 65w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic13-225x88.png 225w, https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-content\/uploads\/sites\/27\/2018\/07\/M32Pic13-350x137.png 350w\" sizes=\"auto, (max-width: 987px) 100vw, 987px\" \/><\/p>\n<p>&nbsp;<\/p>\n<p class=\"hanging-indent\"><strong style=\"text-align: initial; text-indent: 1em; font-size: 1em;\">Conclusions<\/strong><\/p>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\">The communication satellites are essential elements in Mobile Communications. All orbital configurations LEO,\u00a0 MEO and GEO are required for\u00a0 MSS purpose. India has several communication satellite in GEO with various frequency band. The space and Ground segments together are helpful in mobile services in global network. In past 50 years the tremendous growth took place in the satellites field and their service which has potentially increased the data rate as well as band width. Advance multi-beam satellites, along with free space RF and Optical link will govern the future applications in mobile services for seamless connectivity.<\/p>\n<table>\n<tbody>\n<tr>\n<td><strong>you can view video on Mobile communications Satellite systems (Part-1)<\/strong><\/td>\n<td><a href=\"https:\/\/youtu.be\/uIzBLF30nLI\" target=\"_blank\" rel=\"noopener\"><img loading=\"lazy\" decoding=\"async\" class=\"alignnone wp-image-120\" src=\"http:\/\/epgpbooks.inflibnet.ac.in\/wp-content\/uploads\/2018\/11\/download.png\" alt=\"\" width=\"36\" height=\"36\" \/><\/a><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<p class=\"hanging-indent\"><strong>Suggested Reading:<\/strong><\/p>\n<ol>\n<li style=\"text-align: justify;\">Mobile Communication 2nd edition by Jochen Schiller, Pearson education<\/li>\n<li style=\"text-align: justify;\">Mobile Computing by Asoke Talukder, Roopa Yavagal (Tata McGraw Hill)<\/li>\n<li style=\"text-align: justify;\">&#8220;Wireless communication and networking&#8221; by William Stallings<\/li>\n<li style=\"text-align: justify;\">Mobile Cellular Telecommunications \u2014 W.C.Y. Lee, Mc Graw Hill<\/li>\n<li style=\"text-align: justify;\">Wireless Communications \u2013 Theodore. S. Rapport, Pearson Education<\/li>\n<li style=\"text-align: justify;\">Reza B&#8217;Far (Ed), &#8220;Mobile Computing Principles&#8221;, Cambridge University Press.<\/li>\n<\/ol>\n","protected":false},"author":4,"menu_order":28,"template":"","meta":{"pb_show_title":"on","pb_short_title":"","pb_subtitle":"","pb_authors":["miss-suchit-purohit"],"pb_section_license":""},"chapter-type":[],"contributor":[59],"license":[],"class_list":["post-354","chapter","type-chapter","status-publish","hentry","contributor-miss-suchit-purohit"],"part":3,"_links":{"self":[{"href":"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-json\/pressbooks\/v2\/chapters\/354","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-json\/pressbooks\/v2\/chapters"}],"about":[{"href":"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-json\/wp\/v2\/types\/chapter"}],"author":[{"embeddable":true,"href":"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-json\/wp\/v2\/users\/4"}],"version-history":[{"count":15,"href":"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-json\/pressbooks\/v2\/chapters\/354\/revisions"}],"predecessor-version":[{"id":659,"href":"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-json\/pressbooks\/v2\/chapters\/354\/revisions\/659"}],"part":[{"href":"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-json\/pressbooks\/v2\/parts\/3"}],"metadata":[{"href":"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-json\/pressbooks\/v2\/chapters\/354\/metadata\/"}],"wp:attachment":[{"href":"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-json\/wp\/v2\/media?parent=354"}],"wp:term":[{"taxonomy":"chapter-type","embeddable":true,"href":"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-json\/pressbooks\/v2\/chapter-type?post=354"},{"taxonomy":"contributor","embeddable":true,"href":"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-json\/wp\/v2\/contributor?post=354"},{"taxonomy":"license","embeddable":true,"href":"https:\/\/ebooks.inflibnet.ac.in\/itp12\/wp-json\/wp\/v2\/license?post=354"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}