Bazyey, Oleksandr A.Базєй, Олександр Анатолійович2015-04-062015-04-062014Odessa Astronomical Publicationshttps://dspace.onu.edu.ua/handle/123456789/6220The numerical integration of the motion equations of a passive high-orbit fragment with large surface area was performed accounting for the main gravitational perturbations of the Earth, Moon and Sun, as well as the solar radiation pressure. Based on the numerical model of motion in the near-Earth space that accounts for only the most powerful perturbations, a new method for deorbiting artificial celestial bodies from high altitudes is suggested.ennumerical – celestial mechanicsArticle