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 42826U 17042B 25322.42791458 .00010346 00000-0 62966-3 0 9996
2 42826 97.4252 130.5833 0008631 91.5709 268.6510 15.10570359455373
| Epoch (UTC): | 18 November 2025 10:16:11 |
| Eccentricity: | 0.0008631 |
| inclination: | 97.4252° |
| perigee height: | 528 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 130.5833° |
| argument of perigee: | 91.5709° |
| revolutions per day: | 15.10570359 |
| mean anomaly at epoch: | 268.6510° |
| orbit number at epoch: | 45537 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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