A satellite is revolving in a orbit at an altitude 330 km from the surface of the earth . calculate it's orbital velocity and tune period . Given that R = 6370km
M = 5.98 x 10^24 kg
G = 6.67 x 10^-11 Nm²/kg²
M = 5.98 x 10^24 kg
G = 6.67 x 10^-11 Nm²/kg²
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