A satellite orbits the Earth in a geosynchronous orbit around the equator, meaning that its period is 24 hours and it stays above the same location on earth at all times. (G = 6.67 x 10⁻¹¹ Nm²/kg².) What is the radius of its orbit?
GM/r2 = v2/r = w2r
The Attempt at a Solution
I can solve this if the mass of Earth is given but since it isn't I'd like to know if there is a way to solve this without using Earth's mass