If ${v_e}$ is escape velocity and ${v_o}$ is orbital velocity of a satellite for orbit close to the earth's surface, then these are related by

Question

${v_o} = \sqrt {2{v_e}} $

v_o $=$ v_e

${v_e} = \sqrt {2{v_o}} $

${v_e} = \sqrt 2 {v_o}$

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