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A body is imparted a velocitv \( v \) from the surface of the
\( P \) earth. If \( v_{0} \) is orbital velocity and \( v_{e} \) be the escape velocity then for :
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(A) \( v=v_{0} \), the body follows a circular track around the earth.
(B) \( vv_{0} \) but \( v e \), the body follows elliptical path around the earth.
(C) \( vv_{0} \), the body follows elliptical path and returns to surface of earth.
(D) \( vv_{e} \), the body follows hyperbolic path and escapes the gravitational pull of the earth.
(A) A, B
(B) B, C
(C) A, B, C
(D) A, B, C, D
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