View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 41873U 16062E 23333.47387927 .00046792 00000-0 85189-3 0 9991
2 41873 51.6732 354.7030 0007221 20.5572 339.5706 15.48996080390762
Epoch (UTC): | 29 November 2023 11:22:23 |
Eccentricity: | 0.0007221 |
inclination: | 51.6732° |
perigee height: | 415 km |
apogee height: | 424 km |
right ascension of ascending node: | 354.7030° |
argument of perigee: | 20.5572° |
revolutions per day: | 15.48996080 |
mean anomaly at epoch: | 339.5706° |
orbit number at epoch: | 39076 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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