The period of revolution of a geostationary satellite is......

Option A

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 m/s) and an orbital period of 1,436 minutes, which equates to almost exactly one sidereal day (23.934461223 hours).