Satellites orbiting closest to Earth or low Earth orbit satellites often find themselves in Earth's shadow, i.e. they aren't exposed to sunlight so they cannot utilize solar cells during that period. In order to be operational while traveling through the shadow they're equipped with batteries. However, batteries are an extra payload that has to be launched with a satellite in orbit. There is an idea that the satellites could be powered even when they are in part of the orbit in which direct sunlight is obstructed by Earth if another satellite in higher orbit illuminates their solar cells by a beam of laser light, which would consequently reduce payload. Essential element of this charging system is a laser that's able to direct its light beam from a satellite emitting energy to a satellite receiving it. Within the scope of this thesis, we deal with different kinds of laser beams, that is, analysis of beams so that we could determine which one would be the most efficient for charging up the satellite over long distances (through empty space). We will evaluate and compare efficacy of different implementations of Gaussian beams with Bessel beams, and Optical Pin beam, which is a special type of light beam, and it's designed with Airy's functions for minimization of diffraction. The question that we'd like to answer is whether the gains from minimization of diffraction can compensate for the losses that occur when creating needed beams with appropriate phase masks.