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 50U 60009B 25344.58538722 -.00000056 00000-0 27637-3 0 9998
2 50 47.2331 27.1337 0113780 173.1740 187.0627 12.20161860914678
| Epoch (UTC): | 10 December 2025 14:02:57 |
| Eccentricity: | 0.0113780 |
| inclination: | 47.2331° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 27.1337° |
| argument of perigee: | 173.1740° |
| revolutions per day: | 12.20161860 |
| mean anomaly at epoch: | 187.0627° |
| orbit number at epoch: | 91467 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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