The ratio of the time periods of two satellites at heights 3600 km, 13,600 km from the surface of the earth is
Kepler’s law-
Tα(R+h)3/2
T1T2=(R+h1R+h2)3/2=(10,00020,000)3/2
=12.828
A satellite is revolving round the earth in circular orbit at some height above surface of earth. It takes 5.26× 103 seconds to complete a revolution while its centripetal acceleration is 9.92 m/s2 . Height of satellite above surface of earth is (Radius of earth 6.37×106 m)