Orbital Mean Elements (OMM)

SatKit supports propagating Orbital Mean-Element Message (OMM) records directly through satkit.sgp4.

OMM input is expected as a dictionary in the same structure used by CelesTrak or Space-Track responses.

satkit.sgp4(tle, time, **kwds)

Runs SGP4 propagation for one or more TLE/OMM inputs at one or more times.

Use this page when your workflow starts from OMM/JSON records instead of Two-Line Elements.