MCQ
A satellite is moving with a constant speed ' $V$ ' in a circular orbit about the earth. An object of mass ' $m$ ' is ejected from the satellite such that it just escapes from the gravitational pull of the earth. At the time of its ejection, the kinetic energy of the object is
- A$\frac{1}{2} m V^2$
- ✓$m V^2$
- C$\frac{3}{2} m V^2$
- D$2 m V^2$

