Question

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

Answer 1

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

$T^2=(\frac{4\pi^2}{GM})^3$

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)