Taking the square root of each side leaves the following equation for the velocity of a satellite moving about a central body in circular motion where g is 6 673 x 10 11 n m 2 kg 2 m central is the mass of the central body about which the satellite orbits and r is the radius of orbit for the satellite. R orbital radius in meters as measured from the earth s centre of mass. Angular velocity of rotation of the earth and that of the geostationary satellite are invariably in the same direction.
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