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 22285U 92093B 25344.83597490 .00000287 00000-0 17158-3 0 9997
2 22285 71.0200 190.7923 0002127 78.1711 281.9650 14.15428004700589
| Epoch (UTC): | 10 December 2025 20:03:48 |
| Eccentricity: | 0.0002127 |
| inclination: | 71.0200° |
| perigee height: | 839 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 190.7923° |
| argument of perigee: | 78.1711° |
| revolutions per day: | 14.15428004 |
| mean anomaly at epoch: | 281.9650° |
| orbit number at epoch: | 70058 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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