A body is moving in a low circular orbit about a planet of mass $M$ and radius $R$. The radius of the orbit can be taken to be $R$ itself. Then the ratio of the speed of this body in the orbit to the escape velocity from the planet is:\\
(1) $\frac { 1 } { \sqrt { 2 } }$\\
(2) 2\\
(3) 1\\
(4) $\sqrt { 2 }$