Indirect Optimization of Satellite Deployment into a Highly Elliptic Orbit

Table 1

Initial and final orbit characteristics.

	𝑎, km	𝑒	𝑖, deg	Ω, deg	𝜔, deg	𝜈
Initial	98922	0.931985	5.2	90.0	270.0	0.0
Final	106247	0.798788	—	—	—	180.0