Planetary Satellite Orbiters: Applications for the Moon

Table 2

Coefficients given by [27].

Coefficients
𝐽2	+2.070×10^−4
𝐽3	+4.900×10^−6
𝐽4	+8.000×10^−7
𝐽5	−3.600×10^−6
𝐽6	−1.100×10^−6
𝐽7	−2.870×10^−5
𝐶22	+2.447305×10^−5