If $v_e$ is escape velocity and $v_o$ is orbital velocity of a satellite for orbit close to the Earth's…
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
$v_o=\sqrt{2} v_e$
$v_o=v_e$
$v_e=\sqrt{2 v_o}$
$v_e=\sqrt{2} v_o$
Solution
Orbital velocity of satellite
$v_o=\sqrt{\frac{G M}{R}}$...(i)
and escape velocity of satellite
$v_e=\sqrt{\frac{2 G M}{R}}$...(ii)
Hence, $\quad v_e=\sqrt{2} v_o$