Assume e.g. that in the spacecraft coordinate system, I have a target vector
$ \vec{p_\text{t}} = \begin{pmatrix} -11.980\\ -68.051\\ 55.031 \end{pmatrix}\text{km}$,
which is related to the Earth Mean Equator (EME) J2000 reference frame. I also have the spacecraft offset vector relative to EMEJ2000
$ \vec{p_\text{sc}} = \begin{pmatrix} -262041633.729\\ 115960324.885\\ 89603436.304 \end{pmatrix}\text{km}$,
and its rotation quaternion (in the form $[\text{cos}(a/2), n_x \text{sin}(a/2)$, $n_y \text{sin}(a/2), n_z \text{sin}(a/2)]$)
$ q_\text{sc} = \left( 0.86476171, -0.43595577, -0.05902956, 0.24216783 \right)$,
as well as the offset vector of the spacecraft origin relative to the camera
$ \vec{p_\text{cam}} = \begin{pmatrix} -0.001234\\ -0.000157\\ 0.001390 \end{pmatrix}\text{km}$,
and its rotation quaternion (also in the form $[\text{cos}(a/2), n_x \text{sin}(a/2)$, $n_y \text{sin}(a/2), n_z \text{sin}(a/2)]$)
$ q_\text{cam} = \left( 0.99999815, 0.00009373, 0.00027332, 0.00190238 \right)$.
How can I use this information to calculate the position of the target in image (pixel) coordinates?
The camera has a FOV of $2.208° \times 2.208°$, $2048 \times 2048$ pixels, a resolution of $1.882 \cdot 10^{-5}$rad, a focal length of $0.7173\text{m}$, and a pixel size of $13.5 \cdot 10^{-6}\text{m}$.