Planetary Satellite Orbiters: Applications for the Moon

Table 3

Model given by [28] (LP165P).

Coefficients [29]
𝐽2	+2.032337×10^−4
𝐽3	+8.475900×10^−6
𝐽4	−9.591930×10^−6
𝐽5	+7.154090×10^−7
𝐽6	−1.357770×10^−5
𝐽7	−2.177470×10^−5
𝐽8	−9.674870×10^−6
𝐽9	+1.549600×10^−5
𝐶22	+2.235700×10^−5