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The escape velocity of a body from the s...

The escape velocity of a body from the surface of the earth is `V_e` and the escape velocity of the body from a satellite orbiting at a height 'h' above the surface of the earth is `v_e`' then

A

`v_e=v_e^'`

B

`v_eltv_e^'`

C

`v_egtv_e^'`

D

`v_elev_e^'`

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