Generate CCSDS OEM v2.0 format ephemerides from a state vector with specified time range, reference frame, time system, and optional covariance propagation. Maximum time span is 30 days.
API Key (format: vsp_sk_...)
State vector display ID
Request parameters for OEM generation with configurable propagation settings
End date for ephemeris generation in ISO-8601 format
"2024-01-02T00:00:00Z"
Start date for ephemeris generation in ISO-8601 format
"2024-01-01T00:00:00Z"
Reference frame for position and velocity vectors
GCRF, EME2000, ITRF, TOD, MOD, TEME "GCRF"
Time step between ephemeris points in seconds
60 <= x <= 8640060
Time system for ephemeris timestamps
UTC, TAI, TT, TDB, TCG, TCB, GPS "UTC"
Covariance reference frame for OEM covariance matrices
RTN, TNW "RTN"
Include covariance matrices in the OEM output
false
OEM file generated successfully
The response is of type string.