Calculate a period of revolution of a polar satellite orbiting close to the earth surfar of the earth given R=6400k g=9.8 M/S
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Explanation: Given: Radius of earth = R = 6400 km = 6.4 x 106 m, Time period = T = 27.3 days = 27.3 x 24 x 60 x 60, g = 9.8 m/s6.
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Given: Radius of earth = R = 6400 km = 6.4 x 106 m, Time period = T = 27.3 days = 27.3 x 24 x 60 x 60, g = 9.8 m/s6.
Explanation:
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