To find the orbital eccentricity \( e \) of the moon, we can use the given relation and the hint provided.
From the hint, the eccentricity can be calculated using the formula: \[ e = \frac{ra - rp}{ra + rp} \]
We're given that \( rp = 0.27ra \).
Substituting this into the formula:
- \( ra = ra \)
- \( rp = 0.27ra \)
Now, substituting \( rp \) in the equation for \( e \):
\[ e = \frac{ra - 0.27ra}{ra + 0.27ra} \] \[ e = \frac{ra(1 - 0.27)}{ra(1 + 0.27)} \] \[ e = \frac{1 - 0.27}{1 + 0.27} \] \[ e = \frac{0.73}{1.27} \]
Now, calculating this value: \[ e = 0.57 \]
Thus, the orbital eccentricity \( e \) is \( 0.57 \).
So the correct response is: 0.57