So you have two objects each with momentum $ \boldsymbol{p}_1 = m_1 \boldsymbol{v}_1 $ and $\boldsymbol{p}_2 = m_2 \boldsymbol{v}_2$. Angular momentum is defined from the body positions as $\boldsymbol{L}_1 = \boldsymbol{r}_1 \times \boldsymbol{p}_1$ and $\boldsymbol{L}_2 = \boldsymbol{r}_2 \times \boldsymbol{p}_2 $, all defined from a common origin.
Together you get the total momentum as the sum of the individual parts
$$ \begin{aligned} \boldsymbol{p} & = \boldsymbol{p}_1 + \boldsymbol{p}_2 & \boldsymbol{L} & = \boldsymbol{L}_1 + \boldsymbol{L}_2 \end{aligned}$$
Now it is unclear what the kinematics of the two bodies are, which leads to further simplifications. For example if the two bodies are in orbit around each other, then they both rotate about a common bary-center defined by $$\boldsymbol{r}_C = \frac{ m_1 \boldsymbol{r}_1 + m_2 \boldsymbol{r}_2 }{m_1 +m_2} $$
Now decompose each position as $\boldsymbol{r}_1 = \boldsymbol{r}_C + \boldsymbol{d}_1$ and $\boldsymbol{r}_2 = \boldsymbol{r}_C + \boldsymbol{d}_2$ and note that for the barycenter to be correct you must have $m_1 \boldsymbol{d}_1 + m_2 \boldsymbol{d}_2 = 0$.
If they orbit each other, then they share a common rotational velocity $\boldsymbol{\omega}$ about the barycenter, and the kinematics are as follows:
$$ \begin{aligned} \boldsymbol{v}_1 &= \boldsymbol{v}_C + \boldsymbol{\omega} \times \boldsymbol{d}_1 &
\boldsymbol{v}_2 &= \boldsymbol{v}_C + \boldsymbol{\omega} \times \boldsymbol{d}_2 \end{aligned}$$
Now take the total momentum
$$\require{cancel} \begin{aligned} \boldsymbol{p} & = m_1 \boldsymbol{v}_1 + m_2 \boldsymbol{v}_2 \\
& = m_1 (\boldsymbol{v}_C + \boldsymbol{\omega} \times \boldsymbol{d}_1) + m_2 ( \boldsymbol{v}_C + \boldsymbol{\omega} \times \boldsymbol{d}_2) \\
& = (m_1 + m_2) \boldsymbol{v}_C + \boldsymbol{\omega} \times \cancel{(m_1 \boldsymbol{d}_1 + m_2 \boldsymbol{d}_2 )} \\
& = (m_1 + m_2)\,\boldsymbol{v}_C
\end{aligned} $$
And the total angular momentum about the barycenter
$$ \begin{aligned}
\boldsymbol{L}_C & = \boldsymbol{d}_1 \times \boldsymbol{p}_1 + \boldsymbol{d}_2 \times \boldsymbol{p}_2 \\
& = \boldsymbol{d}_1 \times m_1 (\boldsymbol{v}_C + \boldsymbol{\omega} \times \boldsymbol{d}_1) + \boldsymbol{d}_2 \times m_2 (\boldsymbol{v}_C + \boldsymbol{\omega} \times \boldsymbol{d}_2) \\
& = \cancel{ ( m_1 \boldsymbol{d}_1 + m_2 \boldsymbol{d}_2 )}\times \boldsymbol{v}_C + \boldsymbol{d}_1 \times ( \boldsymbol{\omega}\times \boldsymbol{d}_1) + \boldsymbol{d}_2 \times ( \boldsymbol{\omega}\times \boldsymbol{d}_2) \\
& = \mathbf{I}_1 \boldsymbol{\omega} + \mathbf{I}_2 \boldsymbol{\omega} = ( \mathbf{I}_1 + \mathbf{I}_2 ) \boldsymbol{\omega}
\end{aligned}$$
where $\mathbf{I}_i$ is a 3×3 mass moment of inertia tensor derived from some mathematical trickery by factoring out $\boldsymbol{\omega}$ from $\boldsymbol{d}_i \times ( \boldsymbol{\omega}\times \boldsymbol{d}_i)$.
Now to transfer the angular momentum to the origin you do the following
$$ \boldsymbol{L} = \boldsymbol{L}_C + \boldsymbol{r}_C \times \boldsymbol{p} $$
What is conserved here is $\boldsymbol{L}_C$ not just in magnitude, but in direction also and also $\boldsymbol{p}$ since no external forces are present. As a result $\boldsymbol{L}$ is conserved also. A condition being that $\boldsymbol{r}_C \times \boldsymbol{v}_C = 0 $.
For each body $\boldsymbol{L}_i = \boldsymbol{d}_i \times m_i ( \boldsymbol{\omega} \times \boldsymbol{d}_i )$ is conserved if $\boldsymbol{\omega}\cdot \boldsymbol{d}_i=0$.