(d) Time period $(T)$ of a synchronous satellite around the earth is given by
$T^{2} = \frac{4\pi^{2}r^{3}}{Gm_{e}} \Rightarrow r = \left( \frac{T^{2}Gm_{e}}{4\pi^{2}} \right)^{1/3}$
Substituting the given values, we get
$r = \left\lbrack \frac{(24 \times 60 \times 60)^{2} + 6.67 \times 10^{- 11} \times 5.98 \times 10^{24}}{4 \times \frac{22}{7} \times \frac{22}{7}} \right\rbrack^{1/3}$
$r = 42.08 \times 10^{6}m$
$\therefore\frac{r}{r_{e}} = \frac{42.08 \times 10^{6}m}{6.37 \times 10^{6}m} = 6.6 \Rightarrow r = 6.6r_{e}$