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 28908U 05048A 25131.69429487 .00000048 00000-0 23347-3 0 9999
2 28908 82.4708 204.3952 0007056 355.5393 160.7249 12.55581781888516
| Epoch (UTC): | 11 May 2025 16:39:47 |
| Eccentricity: | 0.0007056 |
| inclination: | 82.4708° |
| perigee height: | 1436 km |
| apogee height: | 1447 km |
| right ascension of ascending node: | 204.3952° |
| argument of perigee: | 355.5393° |
| revolutions per day: | 12.55581781 |
| mean anomaly at epoch: | 160.7249° |
| orbit number at epoch: | 88851 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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