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 57441U 23105M 25321.90098709 .00001011 00000-0 89884-4 0 9991
2 57441 43.0010 149.1607 0001198 269.8639 90.2066 15.02553093128581
| Epoch (UTC): | 17 November 2025 21:37:25 |
| Eccentricity: | 0.0001198 |
| inclination: | 43.0010° |
| perigee height: | 558 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 149.1607° |
| argument of perigee: | 269.8639° |
| revolutions per day: | 15.02553093 |
| mean anomaly at epoch: | 90.2066° |
| orbit number at epoch: | 12858 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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