Solution
If vev_eve denotes escape velocity and v0v_0v0 Denote orbital velocity then relationship between escape and orbital velocity can be expressed as below
vevo=2\frac{v_e}{v_o}=\sqrt{2}vove=2
At the surface of earth
ve=2v0v_e=\sqrt{2}v_0ve=2v0 =1.41vo1.41v_o1.41vo
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