Geostationary Satellite Orbit Speed

A geosynchronous orbit is a high earth orbit that allows satellites to match earth s rotation.

Geostationary satellite orbit speed.

This particular orbit is. This equation represents the speed that a satellite at a given radius must travel in order to orbit if the orbit is due to gravity. Geostationary orbit a circular orbit 35 785 km 22 236 miles above earth s equator in which a satellite s orbital period is equal to earth s rotation period of 23 hours and 56 minutes. A geostationary orbit is a circular orbit directly above the earth s equator approximately 35 786 km above ground.

Assume for planets similar to earth but with different rotation speeds including zero and we put a satellites at altitude of 35 786 km hr similar to the geostationary orbit or earth with speed 11 068 km hr similar to the speed of communication satellites. These satellites can rotate around the center point of the planets at any direction regardless of it s rotation axis as long as it. A geosynchronous orbit sometimes abbreviated gso is an earth centered orbit with an orbital period that matches earth s rotation on its axis 23 hours 56 minutes and 4 seconds one sidereal day the synchronization of rotation and orbital period means that for an observer on earth s surface an object in geosynchronous orbit returns to exactly the same position in the sky after a period. New high speed army satellites accelerate attacks on enemy tanks.

A spacecraft in this orbit appears to an observer on earth to be stationary in the sky. This equation holds for any orbiting object where the attraction is the force of. The smallest inclination that a satellite can be launched into is that of the launch site s latitude so launching the satellite from close to the equator limits the amount of inclination change needed later. Geostationary earth orbit and meo.

Additionally launching from close to the equator allows the speed. What is the speed of the satellite in orbit. Geostationary satellites are launched to the east into a prograde orbit that matches the rotation rate of the equator. Located at 22 236 miles 35 786 kilometers above earth s equator this position is a valuable spot.

The eccentricity and inclination are not bound to specific values although to be synchronous the orbit must not intersect with the atmosphere or surface of the orbited body causing the orbit to change. The period of the satellite is one day or approximately 24. A synchronous orbit is an orbit where the orbital period equals the rotation rate of the orbited body.