Abstract: An orbital debris processor includes a square shaped central lens connected to four square shaped satellite lenses. All of the lenses have substantially the same focal length. The lenses are disposed to cause columnated light, parallel to respective axes thereof, to be focussed a substantially a single point. When the debris procesor is oriented to cause solar radiation to be parallel to the axis of the central lens, reflectors reflect solar radiation to the satellite lenses parallel to respective axes thereof. When a metal object is positioned at the point, it is locally melted and this enables a cut to be made. These cut pieces can be used by the processor or stored in a bin.