(a) When a satellite is moving in on elliptical orbit, it’s angular momentum ($= \overrightarrow{\mathbf{r}} \times \overrightarrow{\mathbf{p}}$) about the centre of earth dos not change its direction. The linear momentum ($= m\overrightarrow{\mathbf{v}}$) does not remain constant as velocity of satellite is not constant. The total mechanical energy of $S$ is constant at all locations.
The acceleration of $S$($=$centripetal acceleration) is always directed towards the centre of earth