A New Constellation Configuration Scheme for Communicating Architecture in Cislunar Space

Figure 15

The inserting trajectory into the nominal orbit near 𝐿𝐿₃ point from the parking orbit with its altitude of 200 km in the syzygy frame. The bounded orbit near 𝐿𝐿₂ point created in full ephemeris model with the epoch time of 12:00, July 1, 2015. Two maneuvers of 3.7585 km/s are required to insert the nominal orbit on the parking orbit and at the end of the Hohmann segment. The transfer duration is 47.57 days.