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Satellite (A) is orbiting earth in a near earth circular orbit of radius 7000Km.
Satellite (B) is orbiting earth in an elliptical orbit with apogee and perigee
distances of 47000Km and 7000Km respectively. Determine the velocities of the
two satellites at point (X). Given (u) = 39.8 x 1013 Nm²/Kg.
Earth
ΣΤΑ
B

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