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 25339.25291940 .00014736 00000-0 27197-3 0 9994
2 25544 51.6297 179.5463 0003586 206.2517 153.8291 15.49328184541691
| Epoch (UTC): | 05 December 2025 06:04:12 |
| Eccentricity: | 0.0003586 |
| inclination: | 51.6297° |
| perigee height: | 416 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 179.5463° |
| argument of perigee: | 206.2517° |
| revolutions per day: | 15.49328184 |
| mean anomaly at epoch: | 153.8291° |
| orbit number at epoch: | 54169 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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