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 \(ℎ_P = \frac{𝑅}{3}\). The accelerations of P and Q due to Earth’s gravity are \(𝑔_P\) and \(𝑔_Q\), respectively. If \(\frac{𝑔_P}{𝑔_Q} = \frac{36}{25}\), what is the value of \(ℎ_Q?\)