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Table 2 The lunar-centered modified classical orbital elements by the retrograde semi-analytical model at LOI epoch

From: Reachable set analysis of practical trans-lunar orbit via a retrograde semi-analytic model

Coordinate systems

\(\kappa_{{{\text{MJ2}}}}\)/m

\(e_{{{\text{MJ2}}}}\)

\(i_{{{\text{MJ2}}}}\)/deg

\(\Omega\)/deg

\(\omega_{{{\text{MJ2}}}}\)/deg

\(f_{{{\text{MJ2}}}}\)/deg

Lunar-centered LVLH

1,849,200

1.19976

127.6819

95.8856(LAN)

149.0733

0

LCF

1,849,200

1.20592

133.4608

273.8549(LAN)

153.3355

0

J2000 Lunar-centered

1,849,200

1.19976

150.0296

50.8816(RAAN)

176.8663

0