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 28485U 04047A 25338.37300723 .00074573 00000-0 12679-2 0 9991
2 28485 20.5535 227.3103 0003554 146.9091 213.1574 15.49721693156411
| Epoch (UTC): | 04 December 2025 08:57:07 |
| Eccentricity: | 0.0003554 |
| inclination: | 20.5535° |
| perigee height: | 415 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 227.3103° |
| argument of perigee: | 146.9091° |
| revolutions per day: | 15.49721693 |
| mean anomaly at epoch: | 213.1574° |
| orbit number at epoch: | 15641 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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