For hyperbolic trajectory of a satellite of mass $m$ having velocity $V$ at a distance $r$
from the center of earth ( $G:$ gravitational constant, $M:$ mass of earth), which one
of the following relations is true?

(A) $\quad \frac{1}{2} m V^{2}>\frac{G M m}{r}$
(B) $\quad \frac{1}{2} m V^{2}<\frac{G M m}{r}$
(C) $\quad \frac{1}{2} m V^{2}=\frac{G M m}{r}$
(D) $\quad \frac{1}{2} m V^{2}<\frac{2 G M m}{r}$

Question ID - 155375 :-

For hyperbolic trajectory of a satellite of mass $m$ having velocity $V$ at a distance $r$
from the center of earth ( $G:$ gravitational constant, $M:$ mass of earth), which one
of the following relations is true?

(A) $\quad \frac{1}{2} m V^{2}>\frac{G M m}{r}$
(B) $\quad \frac{1}{2} m V^{2}<\frac{G M m}{r}$
(C) $\quad \frac{1}{2} m V^{2}=\frac{G M m}{r}$
(D) $\quad \frac{1}{2} m V^{2}<\frac{2 G M m}{r}$

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