In satellite communications, a geosynchronous orbit is a satellite orbit
in which the period of rotation of the satellite is
an integer multiple of the Earth’s period of rotation. The
most common multiple is one, where the satellite's period of
rotation equals the Earth's. A geosynchronous satellite can have any
angle of inclination. The geostationary Earth orbit is a particular
case of a geosynchronous orbit located in the equatorial
plane (with a 0° inclination), and a height (35 786
km) and velocity (3.073 km/s or 11 069 km/hr) such
that the period of rotation equals that of the Earth.
Consequently, a satellite in geostationary orbit appears stationary to Earth
stations beneath it. This is a very useful orbit for
satellite communications systems that require a large coverage area with
little or no pointing required of the Earth station antenna.
Other topics in our resources on Satellite Communications related to Geosynchronous orbit include: