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 57499U 26145.46157742 +.00000000 +00000-0 -15626-3 0 00005
2 57499 43.0068 288.3244 0003021 278.0889 81.9620 15.27601664 00
| Epoch (UTC): | 25 May 2026 11:04:40 |
| Eccentricity: | 0.0003021 |
| inclination: | 43.0068° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 288.3244° |
| argument of perigee: | 278.0889° |
| revolutions per day: | 15.27601664 |
| mean anomaly at epoch: | 81.9620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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