864950.fig.0016
Figure 16: The inserting trajectory into the nominal orbit near point from the parking orbit with its altitude of 200 km in the syzygy frame. The bounded orbit near point created in full ephemeris model with the epoch time of 12:00, July 1, 2015. Two maneuvers of 3.761 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 63.4 days.