Statement A is true: Satellites in the same orbit have the same radius and hence same time period, derived from \( T = 2\pi \sqrt{\frac{r^3}{GM}} \).
Statement B is true: Orbital velocity is \( v = \sqrt{\frac{GM}{r}} \), which implies \( v \propto \frac{1}{\sqrt{r}} \).
Statement C is false: Escape velocity depends on the distance from the center of the Earth, i.e., altitude affects the value. \( v_{esc} = \sqrt{2gR} \) is valid only at surface.