Physics, asked by kumarbidut80, 2 months ago

obtain an expression for the orbital velocity and time period of rotation of a satellite

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Answered by arbgamer001

Answer:

We get v = 7.92 kms-1, the velocity required by the satellite to revolve in an orbit just near the surface of the earth. Putting g = 9.8 ms-2 and R = 6.4 x 106 m in (iv), we get T = 84.6 minutes, that is the time period of a satellite revolving near the surface of the earth.

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