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**1. Homework Statement**

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. Homework Equations**

W

_{NC}=E

_{2}-E

_{1}

F

_{c}=ma

_{c}

**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.