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$\frac{1}{3} m v^2$
- B$mv ^2$
- C$\frac{1}{2} m v^2$
- D$\frac{2}{3} m v^2$

