Ima take another picture of the question cause uh im not good at entering in this type of problem

Fronk asked Jun 23, 2023

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Fronk asked Jun 23, 2023

by Fronk

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18 votes

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

$T^2=((4\pi^2)/(GM))^3$

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

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

Hence, the correct answer is (c)

Kevin Teljeur answered Jun 28, 2023

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