Ap Eapcet
Gravitation
AP EAPCET 2025 - 23rd May Evening Shift
MCQ+1 / -02025
An artificial satellite is revolving around a planet of radius $R$ in a circular orbit of radius ' $a$ '. If the time period of revolution of the satellite. $T \propto a^{3 / 2} g^x R^y$, then the values of $x$ and $y$ are respectively
[ $g=$ acceleration due to gravity]