A satellite has a mass of 5950 kg and is in a circular orbit 3.80 105 m above the surface of a planet. The period of the orbit is two hours. The radius of the planet is 4.15 106 m. What is the true weight of the satellite when it is at rest on the planet's surface

force gravity=force centripetal

weightSurface(radplanet/(radplanet+alt))^2= mass*v^2/(radplanet+alt)

But v= 2PI(radplanet+alt)/period

so put that in for v, and solve for weight surface.