Fig. 1. Application of high energy pulsed solenoids with capacitor power supply in a satellite swarm. Conceptually it is considered that the problem has two components, the foundational physics of multiple fields being wholly functional and the physical components functioning in the proposed orbital environment. Broad literature reviews have concluded that no singular aspect of context or design prevents function so the proposed concept must be viable by conclusion. The electromagnetic analysis of the proposed interaction is the purpose of this paper, component technologies are detailed before the design is assessed in relation to the problem.