If ve is escape velocity and v0 is orbital velocity of a

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If ve is escape velocity and v0 is orbital velocity of a satellite for orbit close to the earth’s surface, then these are related by :

1. v₀ = √2 v_e
2. v₀ = v_e
3. v_e = √2v₀
4. v_e = √2 v₀

Correct Option: D

v_e = √2 v₀