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 is defined by the following mean orbital elements,
1 54860U 26145.42352744 +.00000000 +00000-0 +22893-4 0 00003
2 54860 43.0031 48.4311 0000894 253.8501 106.2252 15.27578397 04
| Epoch (UTC): | 25 May 2026 10:09:52 |
| Eccentricity: | 0.0000894 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 48.4311° |
| argument of perigee: | 253.8501° |
| revolutions per day: | 15.27578397 |
| mean anomaly at epoch: | 106.2252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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