Searching For Optimal Areas of Circumlunar Space for Placement of Satellites Moving in Circular Orbits
摘要
Orbital evolution of model circumlunar objects moving in circular orbits is analyzed to determine areas optimal for the deployment of new satellite systems moving in orbits of this kind. The areas are determined in which the objects not only remain in their orbits for a long time, but also keep preset initial parameters and hence are the most suitable for the deployment of long-living satellite systems.