A satellite is taken to a height ‘h’ above earth’s surface and imparted a transverse velocity $\upsilon$  . Depending upon imparted velocity $\upsilon$ , different types of satellite motion are possible. In List-I, velocities are enlisted, in List-II possible trajectories are enlisted. (Take,  $V_0=\sqrt{\frac{GM}{R+h}}$ ;  $V_e=\sqrt{\frac{2GM}{R+h}}$ ; where M and R are mass and radius of earth respectively)

List I		List II
I)	$v<v_0$	P)	Elliptical trajectory, point of projection being APOGEE of ellipse
II)	$v_0<v<v_e$	Q)	Elliptical trajectory, point of projection being PERIGEE of ellipse
III)	$v=v_e$	R)	Parabolic trajectory, satellite escaping from earth’s gravitational field
IV)	$v>v_e$	S)	Hyperbolic trajectory, satellite escaping from earth’s gravitational field