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Newton's Law of Gravitation

a satellite r...

Question

a satellite rotating very close to the surface of the earth has approximate linear speed equal to a. 7km/s b. 8km/s

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Q. For a satellite very close to the earth surface

h << R_{e}

i . e . r = R_{e}

v_{0} = \sqrt{\frac{G M}{R_{e}}} + \sqrt{g R_{e}} = 8 k m / s e c

Q. For a satellite very close to surface of earth, we get time period of satellite equal to

Q. For a satellite very close to the surface of earth, we get the time period of the satellite equal to

If a satellite is orbiting the earth very close to its surface, then the orbital velocity mainly depends on

Q. If a satellite is revolving very close to the surface of earth, then its orbital velocity does not depend upon.

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