To find the minimum speed, the satellite must just be able to reach the null point (where the gravitational forces of the two planets cancel out) with zero kinetic energy. After this point, the gravity of the second planet will pull it in.
Let the null point be at a distance x from the center of the first planet (mass M). The distance from the second planet (mass 9M) will be (8R - x).
At the null point, the net gravitational force is zero:
$\frac{G M m}{x^2} = \frac{G (9M) m}{(8R - x)^2}$
$\frac{1}{x^2} = \frac{9}{(8R - x)^2} \implies \frac{1}{x} = \frac{3}{8R - x}$
$8R - x = 3x \implies 4x = 8R \implies x = 2R$.
Now, we apply the principle of conservation of energy. The initial energy at the surface of the first planet must equal the final energy at the null point.
Initial Energy ($E_i$) at the surface of the first planet:
$E_i = K.E._{initial} + P.E._{initial} = \frac{1}{2}mv^2 - \frac{GMm}{R} - \frac{G(9M)m}{(8R-R)} = \frac{1}{2}mv^2 - \frac{GMm}{R} - \frac{9GMm}{7R}$
Final Energy ($E_f$) at the null point (with minimum speed, so $v_{final}=0$):
$E_f = K.E._{final} + P.E._{final} = 0 - \frac{GMm}{x} - \frac{G(9M)m}{(8R-x)} = -\frac{GMm}{2R} - \frac{9GMm}{6R} = -\frac{GMm}{2R} - \frac{3GMm}{2R} = -\frac{4GMm}{2R} = -\frac{2GMm}{R}$
By conservation of energy, $E_i = E_f$:
$\frac{1}{2}mv^2 - \frac{GMm}{R} - \frac{9GMm}{7R} = -\frac{2GMm}{R}$
Divide by m and rearrange:
$\frac{1}{2}v^2 = \frac{GM}{R} + \frac{9GM}{7R} - \frac{2GM}{R} = GM \left( \frac{1}{R} + \frac{9}{7R} - \frac{2}{R} \right)$
$\frac{1}{2}v^2 = \frac{GM}{R} \left( \frac{7+9-14}{7} \right) = \frac{GM}{R} \left( \frac{2}{7} \right)$
$v^2 = \frac{4GM}{7R} \implies v = \sqrt{\frac{4GM}{7R}}$
Comparing this with the given expression $v = \sqrt{\frac{aGM}{7R}}$, we get $a=4$.