Mission Planning of GEO Active Debris Removal Based on Revolver Mode

Table 3

Initial orbital elements of debris.

Serial number	Inclination (°)	RAAN (°)	True anomaly (°)
SD1	5	110	15
SD2	7	280	46
SD3	6.5	125	94
SD4	4	5	138
SD5	5	70	162
SD6	6.8	95	217
SD7	4	145	239
SD8	8	15	277
SD9	4.7	55	334