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 15517U 85013B 25339.95483148 .00000042 00000-0 23730-4 0 9995
2 15517 82.5345 137.5522 0015582 138.4653 221.7695 13.84994691 63256
| Epoch (UTC): | 05 December 2025 22:54:57 |
| Eccentricity: | 0.0015582 |
| inclination: | 82.5345° |
| perigee height: | 935 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 137.5522° |
| argument of perigee: | 138.4653° |
| revolutions per day: | 13.84994691 |
| mean anomaly at epoch: | 221.7695° |
| orbit number at epoch: | 6325 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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