Take v = velocity given to satellite in a direction perpendicular to its radial distance R, ${\mathrm{v}}_0=\sqrt{\frac{\mathrm{GM}}{\mathrm{R}}},\hspace{0.17em}\hspace{0.17em}{\mathrm{V}}_{\mathrm{e}}=\mathrm{escape}\hspace{0.17em}\hspace{0.17em}$velocity

	List I		List II
(A)	$\mathrm{V}={\mathrm{V}}_0$	(P)	Elliptical path
(B)	${\mathrm{V}}_0<\mathrm{V}<{\mathrm{V}}_{\mathrm{e}}$	(Q)	Hyperbolic path
(C)	$\mathrm{V}={\mathrm{V}}_{\mathrm{e}}$	(R)	Circular path
(D)	$\mathrm{V}>{\mathrm{V}}_{\mathrm{e}}$	(S)	Parabolic path