"In this regard, at the preliminary design stage, the possibilities and feasibility of using an OS analogue in orbits with an inclination of 97° and an altitude of up to 400 km should be considered. If this issue is resolved positively, the scope of modifications to the RLA-120 launch vehicle, specific tasks that the system can solve, based on the characteristics of the OS analogue and the conditions for launching the launch vehicle, must also be determined."