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=((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)