What would be the period of a satellite in a low orbit around this large dense planet yahoo
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For the movement of a satellite around a planet: V = square (GM) / R), where G is gravity constant, M is the mass of the planet, and R is the radius of the orbit.
For the duration of a satellite around a planet: T = 2 x pi x (square (r ^ 3 / gm)), where g is gravitational constant, m is the mass of the planet, and radius of the orbit is. In both cases, R is the distance from the planet's center; Not only the height on its surface
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