So we can hold the factors other than d unitary to determine the relative strengths at the following distances (truncated for space):~380k km (roughly the moon's average distance) = 6.925e-12~36000 km (typical geosynchronous orbit, ie, GPS) = 7.716e-10~2000 km (medium earth orbit) = 2.5e-7So an object at MEO has 324x as much pull as the same object at typical geosynchronous distance, and >36000x a