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Homework Statement
Using a development similar to Kepler's law of periods for planets orbiting the Sun, find the required altitude of geosynchronous satellites above the earth.
Homework Equations
(R^3)/T^2=(G*M)/(4pi^2)
The Attempt at a Solution
I'm honestly not even sure where to start. The correct answer is supposed to be 3.59*10^7m above the surface.