# Mean orbital elements and explicit ephemeris samples are imported as data. meanOrbit = omm"""CCSDS_OMM_VERS = 3.0 CREATION_DATE = 2026-10-30T00:00:00Z ORIGINATOR = Grid fixture OBJECT_NAME = Example OBJECT_ID = 2026-001A CENTER_NAME = EARTH REF_FRAME = TEME TIME_SYSTEM = UTC MEAN_ELEMENT_THEORY = SGP4 EPOCH = 2026-303T00:00:00Z MEAN_MOTION = 15.5 [rev/day] ECCENTRICITY = 0.001 INCLINATION = 51.6 [deg] RA_OF_ASC_NODE = 20 [deg] ARG_OF_PERICENTER = 30 [deg] MEAN_ANOMALY = 40 [deg] NORAD_CAT_ID = 9007199254740993 BSTAR = 0 MEAN_MOTION_DOT = 0 MEAN_MOTION_DDOT = 0 USER_DEFINED_LABEL = Résumé """ # XML unit and time-system assistance follows the same reader vocabulary. ephemeris = oem"""

2026-10-30T00:00:00Z Grid fixture

Example 2026-001A EARTH EME2000 UTC 2026-10-30T00:00:00Z 2026-10-30T00:00:00Z Résumé 2026-10-30T00:00:00Z 7000 0 0 0 7.5 0 -0.008 0 0 """ meanElements = meanOrbit.elements ephemerisSegments = ephemeris.segments