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If ve is escape velocity and vo is orbital velocity of a satellite for orbit close to the earth's surface, then these are related by :

a
ve=2v0
b
ve=2v0
c
v0=2ve
d
vo = ve

detailed solution

Correct option is B

Escape velocity ve=2GMROrbital velocity (near earth's surface) v0=GMRSo, ve=2v0

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