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 25544U 98067A 25348.86277765 .00007299 00000-0 13766-3 0 9993
2 25544 51.6306 131.9662 0003207 249.8734 110.1909 15.49595360543189
| Epoch (UTC): | 14 December 2025 20:42:23 |
| Eccentricity: | 0.0003207 |
| inclination: | 51.6306° |
| perigee height: | 416 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 131.9662° |
| argument of perigee: | 249.8734° |
| revolutions per day: | 15.49595360 |
| mean anomaly at epoch: | 110.1909° |
| orbit number at epoch: | 54318 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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