
Arturo O. answered 12/07/16
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Suppose a satellite of mass m is orbiting a planet of mass M, along a circular path of radius r, with the planet at the center of the circle. Set the gravitational force between the planet and satellite equal to the centripetal force on the satellite. You can do this because the gravitational force keeps the satellite on the circular path.
GMm/r2 = mv2/r
Note that m appears on both sides and therefore is canceled out.
GM/r2 = v2/r = ac
ac = centripetal acceleration
Note that ac depends on the mass of the planet, but not on the mass of the satellite.