Two satellite A and B , ratio of masses `3 : 1` are in circular orbits of radii r and 4 r . Then ratio of total mechanical energy of A to B is

Two satellites P and Q ratio of masses 3:1 are in circular orbits of radii r and 8r . Then ratio of total mechanical energy of A to B is

Two satellites P and Q ratio of masses 3:1 are in circular orbits of radii r and 8r . Then ratio of total mechanical energy of A to B is

Two satellite A and B, ratio of masses 3:1 are in circular orbits of radii r and 4r . Then ratio mechanical energy of A and B is

Two satellites of masses 3 m and m orbit the earth in circular orbits of radii r and 3 r respectively. The ratio of the their speeds is

Two satellite fo masses m and 4m orbit the earth in circular orbits of radii 4r and r respectively. The ratio of their orbital speed is

Two satellite fo masses m and 4m orbit the earth in circular orbits of radii 4r and r respectively. The ratio of their orbital speed is

Statement-1 : Two satellites of mass 3 M and M orbit the earth in circular orbits of radii r and 3r respectively. The ratio of their speeds is sqrt(3) : 1 . Statement-2 : Orbital velocity of satellite is upsilon = sqrt((GM)/(r ))