The linear velocity of each of point p and s is given by angular velocity times the distance of them from center of earth which is different for. 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. Angular velocity of rotation of the earth and that of the geostationary satellite are invariably in the same direction.
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