Indirect Optimization of Satellite Deployment into a Highly Elliptic Orbit

Table 3

Characteristics of the 4.5-revolution transfer with departure on December 1, 2015.

𝑃𝑓	𝑡2−𝑡1	𝑡4−𝑡3	𝑡6−𝑡5	𝑡8−𝑡7	𝑚𝑓
	hr	hr	hr	hr	kg
0.0	0.09	2.87	2.83	2.79	845.57
0.2	0.09	3.59	2.75	2.16	845.40
0.4	0.09	4.27	2.79	1.45	845.25
0.6	0.09	4.97	2.96	0.59	845.10
0.8	0.09	5.51	3.02	—	844.96
1.0	0.09	5.84	2.70	—	844.83