Semianalytic Integration of High-Altitude Orbits under Lunisolar Effects

Table 6

Initial conditions in the single- (top) and double-averaged phase space (bottom) after different truncation orders 𝑛 of the semi-analytical theory. Distances are km, and angles are deg.

𝑛	28560−𝑎	0.2−𝑒	56−𝑖	0−𝜔	72−Ω	0−ℓ
4	3.06217	0.0000723	0.0014902	0.0000000	0.0000000	0.0000000
5	3.06923	0.0000722	0.0014713	−0.0016703	0.0000132	0.0016800
6	3.06073	0.0000720	0.0014808	−0.0017529	0.0000081	0.0018807
7	3.06077	0.0000720	0.0014820	−0.0017477	0.0000075	0.0018817
8	3.06085	0.0000721	0.0014819	−0.0017510	0.0000042	0.0018783
4	3.06073	0.0000453	−0.0030387	−0.0149534	−0.0027445	0.0167622
5	3.06923	0.0000431	−0.0026903	−0.0153934	−0.0028968	0.0172767
6	3.06073	0.0000432	−0.0026846	−0.0153427	−0.0029047	0.0173255
7	3.06077	0.0000432	−0.0026744	−0.0153287	−0.0028995	0.0173220
8	3.06085	0.0000433	−0.0026745	−0.0153319	−0.0029027	0.0173187