Preliminary Design of Debris Removal Missions by Means of Simplified Models for Low-Thrust, Many-Revolution Transfers

Table 4

Relative inclination change |Δ𝑖| (deg) between orbit planes of the debris.

Debris number	2	3	4	5
1	2.16	1.47	1.95	1
2	—	3.63	2.65	2
3	—	—	2.52	2
4	—	—	—	1