Answer:
Option B
Explanation:
In circular orbit of a satellite, potential energy
$=-2 \times $(kinetic energy)
=$-2 \times \frac{1}{2} mv^{2}=-mv^{2}$
Just to escape from the gravitational pull, its total mechanical energy should
be zero. Therefore' its kinetic energy should be $+mv^{2}$
$\therefore$ Correct answer is (b)