<P> A geostationary orbit can be achieved only at an altitude very close to 35,786 km ( 22,236 mi ) and directly above the equator . This equates to an orbital velocity of 3.07 km / s ( 1.91 mi / s ) and an orbital period of 1,436 minutes , which equates to almost exactly one sidereal day ( 23.934461223 hours ) . This ensures that the satellite will match the Earth 's rotational period and has a stationary footprint on the ground . All geostationary satellites have to be located on this ring . </P>
<P> A geostationary orbit can be achieved only at an altitude very close to 35,786 km ( 22,236 mi ) and directly above the equator . This equates to an orbital velocity of 3.07 km / s ( 1.91 mi / s ) and an orbital period of 1,436 minutes , which equates to almost exactly one sidereal day ( 23.934461223 hours ) . This ensures that the satellite will match the Earth 's rotational period and has a stationary footprint on the ground . All geostationary satellites have to be located on this ring . </P>
the orbital speed of geo stationary satellite is
the orbital speed of geo stationary satellite is
3.07 km / s ( 1.91 mi / s )
3.07 km / s ( 1.91 mi / s )