Accepted Answer
The satellite revolves in a circular orbit and has a centripetal acceleration. This centripetal acceleration is caused by the gravitational attraction force of the planet.m = mass of satellite M mass of planet R radius of the orbitV linear velocity tangential to the orbit G = gravitational constantCentripetal force = m V² / R = gRGravitational Force = G Mm / R²So, V² = G M/RSo, M = V² R / G = 500² * 8000 * 1000 / 6.67 * 10^-11 = 2.998 * 10^22 Kg