Semianalytic Integration of High-Altitude Orbits under Lunisolar Effects

Table 2

Inclination coefficients 𝑝_2,𝑗,𝑘 and 𝑝_3,𝑗,𝑘; for brevity, we use the notation 𝛾≡(1±𝑐).

𝑘	𝑝2,0,𝑘	𝑝2,2,𝑘	𝑝3,1,𝑘	𝑝3,3,𝑘
0	(1/8)(2−3𝑠^2)	(15/8)𝑠^2	(15/64)𝑠(1−5𝑐^2)	−(175/64)𝑠^3
±1	(3/4)𝑐𝑠	∓(15/4)𝑠𝛾	(15/256)𝛾(1±10𝑐−15𝑐^2)	−(525/256)𝑠^2𝛾
±2	(3/16)𝑠^2	(15/16)𝛾^2	±(75/256)𝑠𝛾(1∓3𝑐)	±(525/256)𝑠𝛾^2
±2			−(25/256)𝑠^2𝛾	−(175/768)𝛾^3