Everything about Geosynchronous Orbit totally explained
A
geosynchronous orbit is an
orbit around the
Earth with an
orbital period matching the Earth's
sidereal rotation period. This synchronization means that for an observer at a fixed location on Earth, a
satellite in a geosynchronous orbit returns to exactly the same place in the sky at exactly the same time each day. The special case of a geosynchronous orbit that's circular and directly above the
equator is called a
geostationary orbit.
A
semisynchronous orbit has an orbital period of 0.5
sidereal days, for example 11 h 58 min. Relative to the Earth's surface it has twice this period. Examples include the
Molniya orbit and the orbits of the satellites in the
Global Positioning System.
Orbital characteristics
Every satellite in geosynchronous orbit has an average
altitude of about 35,780 km (about 22,233 miles). When the orbit has a non-zero
inclination or
eccentricity, the
ground track of a satellite in that orbit is a more or less distorted figure-eight, returning to the same places once per solar day.
Orbits with the same period share the same semi-major axis:
where a=semi-major axis, P=Period of the orbit, mu=gravitational constant of body being orbited.
Geostationary orbits (a special type of geosynchronous orbit) and geosynchronous orbits both have a period of 24 sidereal hours, therefore both have the same semi-major axis.
Geostationary orbit
A circular geosynchronous orbit in the plane of the Earth's equator has a radius of approximately 42,164 km (from the center of the Earth). A satellite in such an orbit is at an altitude of approximately 35,786 kilometers above
mean sea level. It will maintain the same position relative to the Earth's surface. If one could see a satellite in geostationary orbit, it would appear to hover at the same point in the sky, for example, not exhibit
diurnal motion, while one would see the Sun, Moon, and stars traverse the heavens behind it. This is sometimes called a Clarke orbit. Such orbits are useful for
telecommunications satellites.
A perfect stable geostationary orbit is an ideal that can only be approximated. In practice the satellite will drift out of this orbit (because of perturbations such as the
solar wind,
radiation pressure, variations in the Earth's gravitational field, and the
gravitational effect of the
Moon and
Sun), and thrusters are used to maintain the orbit in a process known as
station-keeping.
Synchronous orbits around general astronomical objects
Synchronous orbits exist around all moons,
planets,
stars and
black holes — unless they rotate so slowly that the orbit would be outside their
Hill sphere or so fast that such an orbit would be inside the body. Most inner moons of planets have
synchronous rotation, so their synchronous orbits are, in practice, limited to their leading and trailing (L4 and L5)
Lagrange points, as well as the L1 and L2 Lagrange points, assuming they don't fall within the body of the moon. Objects with
chaotic rotations (such as
Hyperion) are also problematic, as their synchronous orbits keep changing unpredictably.
Other geosynchronous orbits
Elliptical orbits can be and are designed for
communications satellites that keep the satellite within view of its assigned ground stations or receivers. A satellite in an elliptical geosynchronous orbit will appear to oscillate in the sky from the viewpoint of a ground station, tracing an
analemma in the sky. Satellites in highly elliptical orbits must be tracked by steerable
ground stations.
Theoretically an
active geosynchronous orbit can be maintained if forces other than gravity are also used to maintain the orbit, such as a
solar sail. Such a
statite can be geosynchronous in an orbit different (higher, lower, more or less elliptical, or some other path) from the
conic section orbit formed by a gravitational body. Such devices are still theoretical.
A further form of geosynchronous orbit is obtained by the theoretical
space elevator in which one end of the structure is tethered to the ground, maintaining a longer orbital period than by gravity alone if under tension.
Other definitions of geosynchronous orbit
- Geosynchronous orbit (GEO): a circular orbit, 35786 km above Earth's surface
The following orbits are special orbits that are also used to categorize orbits:
Geostationary orbit (GSO): zero inclination geosynchronous orbit
Supersynchronous orbit - a disposal / storage orbit above GSO/GEO. Satellites will drift in a westerly direction.
Subsynchronous orbit - a drift orbit close to but below GSO/GEO. Used for satellites undergoing station changes in an eastern direction.
Graveyard orbit - a supersynchronous orbit where spacecraft are intentionally placed at the end of their operational life.
History
Author Arthur C. Clarke is credited with proposing the notion of using a geostationary orbit for communications satellites. The orbit is also known as the Clarke Orbit. Together, the collection of artificial satellites in these orbits is known as the Clarke Belt.
The first communications satellite placed in a geosynchronous orbit was Syncom 2, launched in 1963. Geosynchronous orbits have been in common use ever since, in particular for satellite television.
Initially, geostationary satellites also carried international telephone traffic but geostationary orbits are no longer used as much for voice communication and international Internet connectivity, partly due to the inherent disconcerting delay in communicating via a satellite in such a high orbit. It takes electromagnetic waves about a quarter of a second to travel from one end to the other of the link, thus two parties talking via satellite will be subject to about a half second delay in round-trip response.
Nearly all populated land locations on the planet now have terrestrial communications facilities (microwave, fiber-optic), even undersea, with more than sufficient capacity. Satellite telephony is now mainly limited to small, isolated locations that have no terrestrial facilities, such as Canada's arctic islands, Antarctica, the far reaches of Alaska and Greenland, and ships at sea.
Further Information
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