The time period of a satellite is related to the distance from the Earth by Kepler’s third law, which states:
\[
T^2 \propto r^3.
\]
If the satellite is 9 times closer to the Earth than the Moon, the distance ratio is:
\[
r_{\text{satellite}} = \frac{r_{\text{moon}}}{9}.
\]
Thus, the time period of the satellite is related to the time period of the Moon by:
\[
T_{\text{satellite}} = T_{\text{moon}} \cdot \left( \frac{1}{9} \right)^{3/2}.
\]
Since the Moon’s time period is 27 days:
\[
T_{\text{satellite}} = 27 \cdot \frac{1}{3} = 1 \, \text{day}.
\]