Research Article

Semianalytic Integration of High-Altitude Orbits under Lunisolar Effects

Figure 2

Sample long-term propagations for 𝜔 = 0 and Ω = 0 full line, 90 dashed, 180 dotted, and 2 7 0 deg. dash-dotted. (a) Eccentricity variation. (b) Inclination variations.
659396.fig.002a
(a)
659396.fig.002b
(b)