  Cislunar space awareness is of increasing interest to the international
community as Earth-Moon traffic is projected to increase. This raises the
problem of placing satellites optimally in a constellation to provide
satisfactory coverage for said traffic. The Circular Restricted 3 Body Problem
(CR3BP) provides promising periodic orbits in the Earth-Moon rotating frame for
traffic monitoring. This work converts a spatially and temporally varying
traffic coverage requirement into an integer linear programming problem,
attempting to minimize the number of satellites required for the requested
coverage.
