A system and method for detection of anti-satellite vulnerability of an orbiting platform. At least some of the instructions in the stream identify one or more architectural registers from a set of architectural registers. Additionally, a first lamp casing for encapsulating the first light source is further formed with a through hole at one side thereof, and a second lamp casing corresponding to the second light source is assembled within the through hole. The hole injecting electrodes are connected together by an electrical conductor disposed on a side surface of the optical fiber. The back also has a domed configuration with a 12 to 15 foot radius.