TRANS-LUNAR INJECTION
T+00d 00:00— · MISSION ELAPSED FROM TLI
Earth range—
Moon range—
Geocentric speed—
Speed vs Moon—
Lunar altitude—
Mission day—
——
—
Reconstruction of the flown mission: RK4 integration of the Earth–Moon three-body
problem, with the TLI solved so pericynthion and maximum range match NASA's reported values. Planar
two-body-plus-Moon model — real timings differ by a few hours.
TLE CelesTrak · SGP4 satellite.js · Imagery Esri / NASA