The only point hat remains at reset is the north pol point.
starting with the rotation matrix
$$\mathbf S= \left[ \begin {array}{ccc} \cos \left( \psi \right) &-\sin \left(
\psi \right) &0\\ \sin \left( \psi \right) &\cos
\left( \psi \right) &0\\ 0&0&1\end {array} \right]\,
\left[ \begin {array}{ccc} 1&0&0\\ 0&\cos \left(
\varphi \right) &-\sin \left( \varphi \right) \\ 0
&\sin \left( \varphi \right) &\cos \left( \varphi \right)
\end {array} \right]
$$
and the position vector of a point on the sphere surface
$$\mathbf R=r\,\left[ \begin {array}{c} \cos \left( \lambda \right) \cos \left(
\vartheta \right) \\ \cos \left( \lambda \right)
\sin \left( \vartheta \right) \\ \sin \left(
\lambda \right) \end {array} \right]
$$
where $~\lambda~$ is the longitudinal angle and $~\vartheta~$ the azimuth angle.
from here , the transformed vector coordinates are
$$\left[ \begin {array}{c} x\\ y\\
z\end {array} \right]
=\mathbf S^T\,\mathbf R\tag 1$$
solving $~x=0~,y=0~$ you obtain that
$$\varphi=\pm
\arctan\left(\frac{1}{\tan(\lambda)}\right)\quad ,\psi=\vartheta \pm\frac\pi2$$
substitute those results in equation (1) you obtain:
$$ \left[ \begin {array}{c} x\\ y\\
z\end {array} \right]=
\left[ \begin {array}{c} 0\\ 0\\
\pm r\end {array} \right]$$
thus , if you rotate the globe first about the z axes with $~\psi=+\psi(\vartheta)~$ and then rotate about the $~x'~$ axes with $~\varphi=+\varphi(\lambda)~$ the only point that remains at reset is the north pol point.
the rotation matrix $~\mathbf S=\mathbf S(\,\psi(\vartheta)_\pm~,\varphi(\lambda)_\pm\,)~$ is then
$$\mathbf S_+= \left[ \begin {array}{ccc} -\sin \left( \vartheta \right) &-\cos
\left( \vartheta \right) \sin \left( \lambda \right) &\cos \left(
\lambda \right) \cos \left( \vartheta \right) \\
\cos \left( \vartheta \right) &-\sin \left( \vartheta \right) \sin
\left( \lambda \right) &\cos \left( \lambda \right) \sin \left(
\vartheta \right) \\ 0&\cos \left( \lambda \right)
&\sin \left( \lambda \right) \end {array} \right]\\
\mathbf S_-=\left[ \begin {array}{ccc} -\sin \left( \vartheta \right) &-\cos
\left( \vartheta \right) \sin \left( \lambda \right) &-\cos \left(
\lambda \right) \cos \left( \vartheta \right) \\
\cos \left( \vartheta \right) &-\sin \left( \vartheta \right) \sin
\left( \lambda \right) &-\cos \left( \lambda \right) \sin \left(
\vartheta \right) \\ 0&\cos \left( \lambda \right)
&-\sin \left( \lambda \right) \end {array} \right]
$$
$\Rightarrow$
the angular velocity obtained in inertial system
$$\mathbf\omega= \left[ \begin {array}{c} \sin \left( \vartheta \right) \dot\lambda
\\ -\cos \left( \vartheta \right) \dot\lambda
\\ \dot\vartheta \end {array} \right]
$$