write the value of orbital velocity of satellite revolving near the surface of the earth
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Answered by
3
hey mate here is your answer
for any body in a circular orbit, its escape velocity is the sqrt(2)- about 1.414 times- its orbital velocity. for a settellite in low earth orbit its velocity is 7.8 km/sec .escape velocity from earth is 11.2km/sec .
Hope it help u .
Answered by
2
Answer:
6.59×10^6
Explanation:
by using v0=√gR
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