A satellite of mass 1200 kg completes one orbital revolution around the Earth( 6400 km in radius, mass 5.98x1024 kg) in 24.0 hours. Find a) the altitude of the satellite

The drag force, fd, imposed by the surrounding air on a vehicle moving with velocity v is given by fd = cdaρv 2/2 where cd is a constant called the drag coefficient, a is the projected frontal area of the vehicle, and ρ is the air density. an automobile is moving at v = 80 kilometers per hour with cd = 0.28, a = 2.3 m2, and ρ = 1.2 kg/m3.