A First-Order Analytical Theory for Optimal Low-Thrust Limited-Power Transfers between Arbitrary Elliptical Coplanar Orbits

Table 3

Set of terminal orbits.

	Initial orbit 1	Final orbit 1	Initial orbit 2	Final orbit 2	Initial orbit 3	Final orbit 3
𝜀𝑆𝑥^,𝑦^,𝜀=𝑘=1𝜀^𝑘𝑆𝑘𝑥^,𝑦^.(A.2)	1.000	1.050	1.000	1.050	1.000	1.050
𝑥^	0.100	0.105	0.200	0.210	0.500	0.525
𝑦^	0.0	0.0	0.0	0.0	0.0	0.0