If ve and vo represent the escape velocity and orbital velocity of a satellite corresponding to a circular orbit of radius R respectively, then
If ve and vo represent the escape velocity and orbital velocity of a satellite corresponding to a circular orbit of radius R respectively, then
(A) ve = vo
(B) \(\sqrt{2}\)vo = ve
(C) ve = \(\frac{1}{\sqrt{2}}\)vo
(D) ve and vo are not related
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