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 25340.86543100 .00013750 00000-0 25394-3 0 9993
2 25544 51.6304 171.5636 0003497 213.1314 146.9456 15.49374779541942
| Epoch (UTC): | 06 December 2025 20:46:13 |
| Eccentricity: | 0.0003497 |
| inclination: | 51.6304° |
| perigee height: | 416 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 171.5636° |
| argument of perigee: | 213.1314° |
| revolutions per day: | 15.49374779 |
| mean anomaly at epoch: | 146.9456° |
| orbit number at epoch: | 54194 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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