Velocity Of Geostationary Satellite With Respect To Earth Is

How high above the earth s surface must the geostationary satellite be placed into orbit.

Velocity of geostationary satellite with respect to earth is.

A few objects with small inclinations to. ř 363 625 0. The geostationary orbit is a circular orbit directly above the earth s equator. The gravitational force between the satellite and the.

From the relationship f centripetal f centrifugal we note that the mass of the satellite m s appears on both sides geostationary orbit is independent of the mass of the satellite. Circular orbit above the earth s equator and following the direction of the earth s rotation two geostationary satellites in the same orbit a 5 6 view of a part of the geostationary belt showing several geostationary satellites. Those with inclination 0 form a diagonal belt across the image. I was wondering whether relative speed of geostationary satellite with respect to earth is zero or not.

To be geostationary a satellite needs to revolute at the velocity of about 11060 km h or 3075 m s. At this velocity it is synchronous with the earth and becomes geostationary. The geostationary satellite are satellite that look s stationary object in the sky or space they revolve around the earth in such a way that they are not changing thier position with respect to. A satellite in this orbit is known as a geostationary satellite and has an orbital period of one sidereal day 23 hours 56 minutes and 4 seconds which means that it completes one revolution around earth in exactly the same time.

Such orbit is called geostationary orbit. R orbital radius earth s equatorial radius height of the satellite above the earth surface r 6 378 km 35 780 km r 42 158 km r 4 2158 x 107 m speed of the satellite is 3 0754 x 103 m s. A geostationary earth satellite with a mass of 3700kg has the following radius and velocity vectors relative to the center of the earth.