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 56825U 26145.39446957 +.00000000 +00000-0 +11343-4 0 00000
2 56825 43.0036 33.4938 0001138 277.0984 82.9739 15.27584492 09
| Epoch (UTC): | 25 May 2026 09:28:02 |
| Eccentricity: | 0.0001138 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.4938° |
| argument of perigee: | 277.0984° |
| revolutions per day: | 15.27584492 |
| mean anomaly at epoch: | 82.9739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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