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 56823U 26145.37534227 +.00000000 +00000-0 +77939-4 0 00007
2 56823 43.0032 34.2041 0001308 273.3497 86.7206 15.27583260 07
| Epoch (UTC): | 25 May 2026 09:00:29 |
| Eccentricity: | 0.0001308 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 34.2041° |
| argument of perigee: | 273.3497° |
| revolutions per day: | 15.27583260 |
| mean anomaly at epoch: | 86.7206° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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