1. The problem statement, all variables and given/known data A satellite is orbiting 600km above the Earths surface. The free fall speed is 8.21 m/s^2. The radius of Earth is 6400km. What is the satellites speed, and the time interval for one orbit around Earth. 2. Relevant equations v = ((2)(PI)(r))/T ac = rw^2 w = (2)(PI) / T 3. The attempt at a solution 8.21 = 7000w^2 w = .0346 .0346 = (2(PI)) / T T = .76 (2)(PI)(7000) / .76 = 57871.44 I am unsure of what to do or where I went wrong.