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# Relation of escape velocity and orbital velocity ???

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As we know

Escape velocity is given by

$V_e=\sqrt \frac{2GM}{R}$

and Orbital velocity  is given by

$V_0=\sqrt{\frac{GM}{R}}$

So we get Relation of escape velocity and orbital velocity as

$V_0=\frac{V_e}{\sqrt2}$

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