Respuesta :

The formula for the period of orbit of a satellite is given as

[tex]T^2=(\frac{4\pi^2}{GM})^3[/tex]

Rearrange the expression in the terms of radius (r) as

[tex]r=\frac{\sqrt[3]{\text{GMT}^2}}{4\pi^2}[/tex]

Hence, the correct answer is (c)

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