Roman C. answered 10/01/15
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Note that for a circular orbit, the gravity force matches the centripetal force which is F = mv2/r.
For the given satellite it is
F = mv2/r = (1120 kg)(3960 m/s)2 / (3.80×106 m) ≈ 4600 N
Note that the final units are Newtons and that I only kept two significant digits because that is the accuracy of the least accurate piece of information, the orbital radius.