1. The problem statement, all variables and given/known data A satellite in a circular orbit around Earth has a speed of 7.15x103 m/s. Determine, in terms of Earth's radius (radius of earth= 6.38 x106m): a) the distance the satellite is from Earth's centre b) the altitiude of the satellite 2. Relevant equations FG = GMm / r2 Fc = mv2 / r G = 6.67 x 10-11 3. The attempt at a solution I'm seriously unsure on how to even start on this one, because I'm not sure what they mean by 'in terms of Earth's radius.' The answer key says 1.22 rearth for a. Do you have to do this through proportionality and ratios? In terms of writing down the given/known: v = 7.15 x 103 m/s rearth = 6.38 x 106 m Mearth = 5.98 x 1024 kg G = 6.67 x 10-11 Nm2/kg2 I can't figure out the force of gravity because I don't have the mass of the satellite, so that cancels out finding Fc as well since I need the mass for that too. Any help on how to start this would be appreciated, thank you.