A Convex Approach for Trajectory Optimization of Super-Synchronous-Transfer-Orbit Large Launch Systems with Time-Position Constraints

Table 2

Parameters of the mission.

Initial condition	, m/s	-4841.51
	, m/s	-5032.27
	, m/s	-3439.57
	, m	-4.994+06
	, m	4.185+06
	, m	9.065+05
	Flight time in LEO, s	1000
Orbital injection	Semimajor axis, m	40478140
	Eccentricity	0.837489
	Attitude of the perigee, km	200
	Attitude of the apogee, km	68000
	Inclination, deg	27.59
	Longitude of ascending node, deg	335.41
	Argument perigee, deg	226.49
	True anomaly, deg	33.54
	Nominal time of injection, s	1410