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BlueSkyy
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Homework Statement
A spy satellite is in circular orbit around Earth. It makes one revolution in 6.02 hours. (Radius of the Earth=6.371 times 106 m)
(a) How high above Earth's surface is the satellite?
(b) What is the satellite's acceleration?
Homework Equations
v = sqrt(G*M Earth / r)
Kepler's 3rd Law
The Attempt at a Solution
I found the angular velocity to be 2.899 rad/sec...
I really don't know where to start after that