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 57900U 26145.52771976 +.00000000 +00000-0 +16687-3 0 00007
2 57900 43.0028 240.5969 0001710 267.2388 92.8268 15.27579968 04
| Epoch (UTC): | 25 May 2026 12:39:54 |
| Eccentricity: | 0.0001710 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.5969° |
| argument of perigee: | 267.2388° |
| revolutions per day: | 15.27579968 |
| mean anomaly at epoch: | 92.8268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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