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 54866U 26145.11572124 +.00000000 +00000-0 -73322-4 0 00005
2 54866 43.0063 49.5643 0001223 283.9571 76.1145 15.27577757 08
| Epoch (UTC): | 25 May 2026 02:46:38 |
| Eccentricity: | 0.0001223 |
| inclination: | 43.0063° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 49.5643° |
| argument of perigee: | 283.9571° |
| revolutions per day: | 15.27577757 |
| mean anomaly at epoch: | 76.1145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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