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A satellite has a mass of 5959 kg and is in a circular orbit 4.85 × 105 m above the surface of a planet. The period of the orbit is 2.4 hours. The radius of the planet is 4.52 × 106 m. What would be the true weight of the satellite if it were at rest on the planet’s surface?
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generally for circular orbit R you can say \(\large m \omega^2 R = \frac{GMm}{R^2}\) so \(\large GM = \omega^2 R^3 = \left( \dfrac{2\pi}{T} \right)^2 R^3\) if the object were at rest on the planet's surface radius \(r_o\) its weight W would be \(W = \dfrac{GMm}{r_0^2}\large = \left( \dfrac{2\pi}{T} \right)^2 R^3 \dfrac{m}{r_o^2}\)
you have all the numbers you need but you need to be very careful how you use them...
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