Satellite laser ranging provides an opportunity to track spacecraft trajectory fluctuationsas well as contributes to study of Earth’s tectonic motions and parameters ofMoon motions. Routine operations of laser ranging are carried out during night-timewhen noise probability is low. Classical approach for distance estimation includesdistance prediction thus reflected signal is expected to arrive during known time intervalcalled gate, however this is not possible when targeted object trajectory is notknown. In these cases gateless registration mode can be applied, but this mode greatlyreduces signal-to-noise ratio. In this thesis filter for noise event reduction during gatelessor full event registration was successfully developed. The filter is applied duringthe post-processing stage to improve signal-to-noise ratio of gathered data from laserranging. Not only the application of filter resulted in reduction of noise events, butalso it provides an insight whether there is an actual useful signal being emitted fromspacecraft. Investigation of event loss during full registration showed loss probabilityof 7.6% for calculated noise rate of 19 events per 0.01 millisecond. The developedfilter in combination with gateless registration mode opens the door for precipitationaltitude determination.