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 16792U 86046B 25347.99438342 .00000738 00000-0 82302-4 0 9999
2 16792 82.4809 161.1291 0023887 148.2017 212.0647 14.85486269113684
| Epoch (UTC): | 13 December 2025 23:51:54 |
| Eccentricity: | 0.0023887 |
| inclination: | 82.4809° |
| perigee height: | 595 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 161.1291° |
| argument of perigee: | 148.2017° |
| revolutions per day: | 14.85486269 |
| mean anomaly at epoch: | 212.0647° |
| orbit number at epoch: | 11368 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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