ORACLE

OBJECTS TRACKED · TLE @ CELESTRAK
LIVE · SGP4 PROPAGATION
--:--:--
UTC · LIVE
--:--:-- IST ·
−12 hlive+12 h
GROUND STATIONnot set
NEXT PASSES · ABOVE 10°
Set a location to see overhead passes.
ISS
LAYERS
Altitude
Velocity
Latitude
Longitude
Orbital period
EARTH
MOON
ORION
CLOSEST APPROACH
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
— fps
Acquiring orbital elements…