MCQ
An artificial satellite revolves around a planet for which gravitational force $(F)$ varies with distance $r$ from its centre as $F \propto r^2$. If $v_0$ its orbital speed, then
- A$v_0 \propto r^{-1 / 2}$
- ✓$v_0 \propto r^{3 / 2}$
- C$v_0 \propto r^{-3 / 2}$
- D$v_0 \propto r$

