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kraigballa
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Homework Statement
A satellite has a mass of 5700 kg and is in a circular orbit 4.2 multiplied by 10^5 m above the surface of a planet. The period of the orbit is two hours. The radius of the planet is 4.25 multiplied by 10^6 m. What is the true weight of the satellite when it is at rest on the planet's surface?
Homework Equations
G = gravitational constant
Me = Mass of planet
r1 = radius from planet to satellite
r2 = radius of planet
v = velocity of satellite in orbit
Fc = centripetal force
T = Time
Fc = msat*v^2/r
G*msat*Me/r^2 = msat*v^2/r
v = Sq. Root(G*Me/r)
The Attempt at a Solution
r1 = 4.67e^6
r2 = 4.25e^6
T = 7200seconds
so v1 = 2*pie*r1/T = 4075.343803 m/s
so Me = v^2 * r1/G = 1.1628389e^24
not sure how to find mass of satellite on planet from here...