1. The problem statement, all variables and given/known data http://i241.photobucket.com/albums/ff4/alg5045/MUG_co_6.jpg A satellite that goes around the earth once every 24 hours is called a geosynchronous satellite is in an equatorial orbit, its position appears stationary with respect to a ground station, and it is known as a geostationary satellite. Find the radius R of the orbit of a geosynchronous satellite that circles the earth. (Note that R is measured from the center of the earth, not the surface) You may use the following constants: G=6.67*10^-11 mass of the earth = 5.98*10^24 kg radius of the earth = 6.38*10^6 m 2. Relevant equations 3. The attempt at a solution I have no idea how to even begin this problem.