Show that for a satellite in a circular orbit of period around Earth (mass )

PHYSICS · Subjective · CBSE · Physics · Gravitation · Gravitation

Problem

Show that for a satellite in a circular orbit of period TT around Earth (mass MM), the orbital radius rr is given by r=(GMT24π2)1/3.r = \left( \dfrac{G M T^{2}}{4\pi^{2}} \right)^{1/3}.

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