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please help me answer this question PHY Homework.
• Equations are in a separate document entitled Equations for Rotational Dynamics Assignment • Moments of inertia formulas
In the diagram below, a satellite orbits Earth in a circular equatorial geosynchronous orbit. Its center of mass orbits h met
d) (10 pts) Derive an equation for the speed of a geosynchronous satellite in terms of G. Mg, and T. Your final equation must
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h. Granttalional force Ege - G MER @ Centripetal force Fe= me2 (Reth) (RE+h)? T Satellite tangential speed uz 2 (REth) for ere) G-6.68x10 SI unit. M6 - 6 X10 6x0kg 1 Then som - 24 h = 24x2600$, 24 - 1 6x10 2 11 * 6-67X10 x 24x3600 Y3 10 2.91x10 mla.

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