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State Vectors
Export a state vector as OMM
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.
GET
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Authorizations
API Key (format: vsp_sk_...)
Path Parameters
State vector display ID
Query Parameters
Time system for OMM epoch timestamp
Available options:
UTC, TAI, TT, TDB, TCG, TCB, GPS Reference frame for mean orbital elements
Available options:
GCRF, EME2000, ITRF, TOD, MOD, TEME Epoch for OMM generation (ISO-8601). Defaults to state vector epoch.
Response
OMM file generated successfully
The response is of type string.