Two satellites \( P \) and \( Q \) are moving in different circular orbits around the Earth (radius \( R \)). The heights of \( P \) and \( Q \) from the Earth surface are \( h_P \) and \( h_Q \), respectively, where \( h_P = R/3 \). The accelerations of \( P \) and \( Q \) due to Earth’s gravity are \( g_P \) and \( g_Q \), respectively. If \( g_P / g_Q = 36 / 25 \), what is the value of \( h_Q \)?
