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 54859U 26145.41581789 +.00000000 +00000-0 +28089-4 0 00006
2 54859 43.0044 48.3751 0001260 252.7792 107.2922 15.27577796 08
| Epoch (UTC): | 25 May 2026 09:58:46 |
| Eccentricity: | 0.0001260 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 48.3751° |
| argument of perigee: | 252.7792° |
| revolutions per day: | 15.27577796 |
| mean anomaly at epoch: | 107.2922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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