The orbital period \(T\) of a satellite is inversely proportional to the square root of the mean radius \(r\) (which includes Earth's radius \(R\) plus altitude \(h\)). The relationship is given by Kepler's third law:
\[T \propto \frac{1}{\sqrt{r}}, \quad \text{where} \quad r = R + h\]
The larger the altitude \(h\), the larger the distance \(r\) from the center of Earth, and the longer the orbital period \(T\) will be. Thus, we arrange the satellites in increasing order of \(r\) (and increasing orbital period \(T\)) based on their given values of \(h\):
- \(h_3 = R/5\) corresponds to the smallest altitude, hence the shortest period.
- \(h_2 = R/4\) gives the second smallest altitude.
- \(h_1 = R/3\) corresponds to a larger altitude and hence a larger period.
- \(h_4 = R/2\) gives the largest altitude and the longest period.
Thus, the correct order is: \((\text{C}), (\text{B}), (\text{A}), (\text{D})\).