Precise Analytical Computation of Frozen-Eccentricity, Low Earth Orbits in a Tesseral Potential

Table 1

Inclination polynomials 𝑞^′_𝑚,𝑗 in (21) and 𝑑^′_𝑚,𝑗 in (28).

𝑞^′0,0=316(19−54𝑐^2−69𝑐^4)	𝑑^′0,0=𝑞^′0,0−34(1−3𝑐^2)^2
	𝑑^′1,09=−4(1−3𝑐^2)^2
𝑞^′2,09=−16(5−18𝑐^2+5𝑐^4)	𝑑^′2,0=𝑞^′2,0
𝑞^′2,29=−16(2−30𝑐^2)𝑠^2	𝑑^′2,2=𝑞^′2,2