For a 2050 kg satellite to have geosynchronous orbit it must have the same periodicity as the Earth which is 24 hours. What altitude above the Earth’s surface does the satellite orbit to
maintain geosynchronous orbit and what is its tangential velocity?
G = 6.67 x 10 -11 M earth = 5.98 x 10 24 kg r earth = 6.38 x 10 6 m