- Geosynchronous satellite
A geosynchronous satellite is a
satellitewhose orbital track on the Earth repeats regularly over points on the Earth over time. If such a satellite's orbit lies over the equatorand the orbit is circular, it is called a geostationary satellite. The orbits of the satellites are known as the geosynchronous orbitand geostationary orbit. Another type of geosynchronous orbit is the Tundra elliptical orbit.
A geosynchronous network is a communication network based on communication with or through geosynchronous satellites.
According to Kepler's Third Law, the orbital period of a satellite in a circular
orbitincreases with increasing altitude. Space stations and Shuttles in Low Earth orbit(LEO), typically two or four hundred miles above the Earth's surface make between fifteen and sixteen revolutions per day. The Moon, at an altitude of about 235,000 miles (378,000 km), takes about 27 days to make a complete revolution [http://nssdc.gsfc.nasa.gov/planetary/factsheet/moonfact.html] . Between those extremes lies the "magic" altitude of 22,300 miles (35,786 km) at which a satellite's orbital periodmatches, or is an integral part of, the period at which the Earth rotates: once every sidereal day(23 hours 56 minutes). In that case, the satellite is said to be "geosynchronous".
If a geosynchronous satellite's orbit is not exactly aligned with the
equator, the orbit is known as an inclined orbit. It will appear (when viewed by someone on the ground) to oscillate daily around a fixed point in the sky. As the angle between the orbit and the equator decreases, the magnitude of this oscillation becomes smaller; when the orbit lies entirely over the equator, the satellite remains stationary relative to the Earth's surface – it is said to be "geostationary".
There are approximately 300 operational geosynchronous satellites.
Geostationary satellites appear to be fixed over one spot above the equator. Receiving and transmitting antennas on the
earthdo not need to track such a satellite. These antennas can be fixed in place and are much less expensive than tracking antennas. These satellites have revolutionized global communications, television broadcastingand weather forecasting, and have a number of important defense and intelligenceapplications.
One disadvantage of geostationary satellites is a result of their high altitude: radio signals take approximately 0.25 of a second to reach and return from the satellite, resulting in a small but significant signal delay. This delay increases the difficulty of
telephoneconversation and reduces the performance of common network protocols such as TCP/IP, but does not present a problem with non-interactive systems such as television broadcasts. There are a number of proprietary satellite data protocols that are designed to proxy TCP/IP connections over long-delay satellite links -- these are marketed as being a partial solution to the poor performance of native TCP over satellite links. TCP presumes that all loss is due to congestion, not errors, and probes link capacity with its " slow-start" algorithm, which only sends packets once it is known that earlier packets have been received. Slow start is very slow over a path using a geostationary satellite.
Another disadvantage of geostationary satellites is the incomplete geographical coverage, since ground stations at higher than roughly 60 degrees latitude have difficulty reliably receiving signals at low elevations.
Satellite dishes in the Northern Hemispherewould need to be pointed almost directly towards the horizon. The signals would have to pass through the largest amount of atmosphere, and could even be blocked by land topography, vegetation or buildings. In the USSR, a practical solution was developed for this problem with the creation of special Molniya/ Orbitainclined path satellite networks with elliptical orbits. Similar elliptical orbits are used for the Sirius Radiosatellites.
The concept was first proposed by
Herman Potočnikin 1928and popularised by the science fiction author Arthur C. Clarkein a paper in Wireless World in 1945. Working prior to the advent of solid-state electronics, Clarke envisioned a trio of large, manned space stations arranged in a triangle around the planet. Modern satellites are numerous, unmanned, and often no larger than an automobile.
The first geosynchronous satellite was
Syncom 2, launched on a Delta rocketB booster from Cape Canaveral 26 July, 1963. It was used a few months later for the world's first satellite relayed telephonecall, between U.S. President John F. Kennedyand Nigerian Prime minister Abubakar Tafawa Balewa.
geostationarycommunication satellite was Syncom 3, launched on August 19, 1964with a Delta D launch vehicle from Cape Canaveral. The satellite, in orbit near the International Date Line, was used to telecast the 1964 Summer Olympicsin Tokyoto the United States. It was the first televisionprogram to cross the Pacific ocean.
List of orbits
List of satellites in geosynchronous orbit
* [http://science.nasa.gov/Realtime/JTrack/3D/JTrack3D.html NASA's software for satellite tracking] shows clearly the position of satellites in geosynchronous orbit.
* [http://www.lyngsat.com/ Lyngsat list of satellites in geostationary orbit]
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