MCQ
Two identical satellites $A$ and $B$ are circulating round the earth at the height of $R$ and $2R$ respectively, (where $R$ is radius of the earth). The ratio of kinetic energy of $A$ to that of $B$ is
- A$\frac{1}{2}$
- B$\frac{2}{3}$
- C$2$
- ✓$\frac{3}{2}$

