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 57711U 26145.43797904 +.00000000 +00000-0 +42817-4 0 00001
2 57711 43.0064 44.1682 0002041 260.0984 99.9637 15.27585924 02
| Epoch (UTC): | 25 May 2026 10:30:41 |
| Eccentricity: | 0.0002041 |
| inclination: | 43.0064° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 44.1682° |
| argument of perigee: | 260.0984° |
| revolutions per day: | 15.27585924 |
| mean anomaly at epoch: | 99.9637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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