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 15890U 85058B 23027.75692321 .00000723 00000-0 84233-4 0 9994
2 15890 82.5284 141.4146 0019537 300.8815 59.0478 14.83788756 28915
| Epoch (UTC): | 27 January 2023 18:09:58 |
| Eccentricity: | 0.0019537 |
| inclination: | 82.5284° |
| perigee height: | 604 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 141.4146° |
| argument of perigee: | 300.8815° |
| revolutions per day: | 14.83788756 |
| mean anomaly at epoch: | 59.0478° |
| orbit number at epoch: | 2891 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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