I. Introduction
Contemporary LEO satellite systems use discrete phased array beamforming antennas in satellites and ground terminals [1] . During the LEO overflight situation the LEO antenna beam needs to be continuously kept accurately pointed towards the ground terminals. Conversely, the terminal beams have to follow the satellite overflight trajectory. The antenna steering is typically realized by means of a discrete set of beam pointing vectors, which is caused by the limited beam resolution of the antenna. This always leads to a nonoptimal beam steering. Through the overflight the system controller selects the best suited pointing vector, which optimizes a given target function. Such a target function can be the average carrier to noise ratio (C/N) of all terminals or the maximum data rate among all terminals in range.