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 13154U 82039B 25193.91677199 .00002739 00000-0 17277-3 0 9993
2 13154 81.1838 131.5696 0032536 24.2272 336.0473 15.08353671345472
| Epoch (UTC): | 12 July 2025 22:00:09 |
| Eccentricity: | 0.0032536 |
| inclination: | 81.1838° |
| perigee height: | 519 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 131.5696° |
| argument of perigee: | 24.2272° |
| revolutions per day: | 15.08353671 |
| mean anomaly at epoch: | 336.0473° |
| orbit number at epoch: | 34547 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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