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 28931U 06002A 21026.21244141 .00000145 00000-0 37019-4 0 9995
2 28931 97.8703 7.3235 0002207 88.2733 271.8717 14.62790337800262
Epoch (UTC): | 26 January 2021 05:05:54 |
Eccentricity: | 0.0002207 |
inclination: | 97.8703° |
perigee height: | 682 km |
apogee height: | 686 km |
right ascension of ascending node: | 7.3235° |
argument of perigee: | 88.2733° |
revolutions per day: | 14.62790337 |
mean anomaly at epoch: | 271.8717° |
orbit number at epoch: | 80026 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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