(d) Orbital radius of satellites $r_{1} = R + R = 2R$
$r_{2} = R + 7R = 8R$
$U_{1} = - \frac{GMm}{r_{1}}$ and $U_{2} = - \frac{GMr}{r_{2}}$
$K_{1} = \frac{GMm}{2r_{1}}$ and $K_{2} = \frac{GMm}{2r_{2}}$
$E_{1} = \frac{GMm}{2r_{1}}$ and $E_{2} = \frac{GMm}{2r_{2}}$
$\therefore\ \frac{U_{1}}{U_{2}} = \frac{K_{1}}{K_{2}} = \frac{E_{1}}{E_{2}} = 4$