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 57526U 26145.41026374 +.00000000 +00000-0 -20263-4 0 00001
2 57526 43.0017 288.4374 0001329 270.8392 89.2308 15.27584609 01
| Epoch (UTC): | 25 May 2026 09:50:46 |
| Eccentricity: | 0.0001329 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 288.4374° |
| argument of perigee: | 270.8392° |
| revolutions per day: | 15.27584609 |
| mean anomaly at epoch: | 89.2308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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