Export a state vector in CCSDS OMM v2.0 format with mean Keplerian elements. Uses DSST (Draper Semi-analytical Satellite Theory) for osculating-to-mean element conversion.
Documentation Index
Fetch the complete documentation index at: https://docs.valar.space/llms.txt
Use this file to discover all available pages before exploring further.
API Key (format: vsp_sk_...)
State vector display ID
Time system for OMM epoch timestamp
UTC, TAI, TT, TDB, TCG, TCB, GPS Reference frame for mean orbital elements
GCRF, EME2000, ITRF, TOD, MOD, TEME Epoch for OMM generation (ISO-8601). Defaults to state vector epoch.
OMM file generated successfully
The response is of type string.