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 25199.88709242 .00002469 00000-0 15555-3 0 9997
2 13154 81.1837 124.7237 0031844 5.0792 355.0749 15.08384722346379
| Epoch (UTC): | 18 July 2025 21:17:24 |
| Eccentricity: | 0.0031844 |
| inclination: | 81.1837° |
| perigee height: | 519 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 124.7237° |
| argument of perigee: | 5.0792° |
| revolutions per day: | 15.08384722 |
| mean anomaly at epoch: | 355.0749° |
| orbit number at epoch: | 34637 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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