The Saturn V threw roughly $m=3\times 10^6{\rm kg}$ out its hinder end at a speed of about $v=3{\rm km\,s^{-2}}$. The angular momentum of this mass thrown tangentially to the ground about Earth's center is then $R_\oplus\,m\,v$, where $R_\oplus$ is the Earth's radius. Assuming the Earth to be uniformly dense for a rough figure, its mass moment of inertia about its center is $I=\frac{2}{5}\,M_\oplus\,R_\oplus^2$. If $\Delta\omega$ is the angular speed change wrought by the firing of the rocket, then conservation of system angular momentum is approximately written:
$$I\,\Delta\omega = \frac{2}{5}\,M_\oplus\,R_\oplus^2\,\Delta\omega = R_\oplus\,m\,v$$.
Solve this equation for $\Delta\omega$: it is not large! It will show you that the effect is utterly negligible.