Proof of angular speed of satellite

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What do you know about circular motion? In particular, about centripetal acceleration?
 
Miklagaard said:
The problem is to show that the orbital angular momentum of a geostationary satellite is given by [tex]\omega^2=G{{M}\over{R^{\,3}}}\,,[/tex] where G is the gravitational constant, M is the mass of the earth, and R is the radius of the orbit.

Miklagaard said:

Homework Equations





The Attempt at a Solution



Proof was asked from me. How do i proof it.

In "w^2 sub. uydu", uydu means satellite.

Use Newton's 2nd Law. Equate the gravitational force on the satellite to the product of the satellite's mass times its centripetal acceleration.
 
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