1. The problem statement, all variables and given/known data 1.A satellites are placed in a circular orbit that is 1.43 × 10^8 m above the surface of the earth. What is the magnitude of the acceleration due to gravity at this distance 2. Relevant equations 1.I used G*mE/r^2 3. The attempt at a solution 1. Got an answer of .0195m/s^2 I think I get this and have no idea why it is wrong.