(adsbygoogle = window.adsbygoogle || []).push({}); 1. The problem statement, all variables and given/known data

A satellite orbits earth at an altitude of 325 km above the planet's surface. what is the oribital period? (radius of earth =6.38 x 10 ^ 6 meters, mass of earth = 5.98 x 10^24 kg)

2. Relevant equations

Net force = 4 pi^2r/T^2 Fg=Gm1m2/r^2

3. The attempt at a solution

4pi^2r/T^2 = gm1m2/r^2

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# Homework Help: Circular motion/gravitation

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