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 55581U 26145.46394547 +.00000000 +00000-0 +19228-5 0 00004
2 55581 43.0029 298.5088 0001168 271.8043 88.2675 15.27575689 06
| Epoch (UTC): | 25 May 2026 11:08:04 |
| Eccentricity: | 0.0001168 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 298.5088° |
| argument of perigee: | 271.8043° |
| revolutions per day: | 15.27575689 |
| mean anomaly at epoch: | 88.2675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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