Match the following columns
`{:(,"Column-I",,"Column-II"),("(A)",underset("satellite in circular orbit")("Time period of an earth"),"(p)","Independent of mass of satellite"),("(B)","Orbital velocity of satellite","(q)","Independent of radius of orbit"),("(C)","Mechanical energy of satellite","(r)","Independent of mass of earth"),(,,"(s)","None"):}`

Answer

`(A rarr p,B rarr p,C rarr s)`

Explanation

`T=(2)/(sqrt(GM))r^(3//2),v_(0)=sqrt((GM)/(r))and E=-(GMm)/(2r)`