Posted by Tatiana on Monday, October 11, 2010 at 10:01pm.
V^2/R = GM/R^2 for circular orbits.
Solve for V
R is the distance from the CENTER of the earth. You will need the Earth's radius, 6378 km. For R, add 440 to that and convert to meters.
G is the universal gravity constant. Get to know it.
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