Question

An earth satellite of mass m revolves in a circular orbit at a height h from the surface of the earth. R is the radius of the earth and g is acceleration due to gravity at the surface of the earth. The velocity of the satellite in the orbit is given by(a) $\frac{gR^{2}}{(R+h)}}$(b) g R(c) $\frac{gR}{(R-h)})}$(d) $\sqrt{\frac{gR^{2}}{(R+h)}}$

Answer 1

$\huge\mathfrak\pink{anSwEr}$

option C is correct ✔️✔️

$\huge{\bf{\blue{\fbox{\underline{\color{orange}</p><p>{hoPe\:iT\:heLpS\:!! }}}}}}$

Answer 2

Hello Friend

The answer of u r question

Option.c

Thank you