Satellite revolve in circular orbit at a height of 1000km from earth calculate orbit velocity
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pole gravitation force is 9.782
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orbital velocity =root(GM/R+h)
R+r = 6400 + 1000 = 7400Km
G = 6.67. x 10^(-11)
M = 6 x 10^(24)
so answer is 73.5 m/s
R+r = 6400 + 1000 = 7400Km
G = 6.67. x 10^(-11)
M = 6 x 10^(24)
so answer is 73.5 m/s
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