1. The problem statement, all variables and given/known data what would be the total mechanical energy of a 200 kg satellite in a geosynchronous orbit around the earth? The only known data is the radius of the earth and mass of the earth the mass of the satellite, m=200 kg, it would have a period of T=24h, but i do not know the radius of the orbit. 2. Relevant equations WNC=E2-E1 Fc=mac 3. The attempt at a solution I don't know how to get an answer with out knowing the radius of the orbit. I tried to make use of the period however i would still need the radius as the velocity is dependent on the radius of the orbit. I would appreciate any help.