d
(d)Orbital radius of satellites \({r_1} = R + R = 2R\)
\({r_2} = R + 7R = 8R\)
\({U_1} = \frac{{ - GMm}}{{{r_1}}}\) and \({U_2} = \frac{{ - GMm}}{{{r_2}}}\)
\({K_1} = \frac{{GMm}}{{2{r_1}}}\) and \({K_2} = \frac{{GMm}}{{2{r_2}}}\)
\({E_1} = \frac{{GMm}}{{2{r_1}}}\) and \({E_2} = \frac{{GMm}}{{2{r_2}}}\)
\(\frac{{{U_1}}}{{{U_2}}} = \frac{{{K_1}}}{{{K_2}}} = \frac{{{E_1}}}{{{E_2}}} = 4\)