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This paper presents a system for removal of space debris, which can be placed on geocentric, heliocentric or Sun-synchronous orbit. The system is composed of two parabolic mirrors, a large one and a small one. The concave face of the large parabolic mirror is oriented toward the concave face of the small parabolic mirror. Sunlight is focused by the large parabolic mirror in its focal point. Then, the light rays are reflected by the small parabolic mirror (which has the same focal point as thedoi:10.13111/2066-8201.2018.10.1.4 fatcat:ghr2qjrbmbek5hqcck2qqdup6q