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 $\frac{{g}_{P}}{{g}_{Q}}=\frac{36}{25},$ what is the value of ${h}_{Q}$?

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Two satellites P and Q are moving in different circular orbits around the Earth (radius R). The heights of P and Q from …

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