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 55590U 26145.38798191 +.00000000 +00000-0 +98018-5 0 00002
2 55590 43.0045 291.9829 0001686 268.4140 91.6518 15.27574807 04
| Epoch (UTC): | 25 May 2026 09:18:41 |
| Eccentricity: | 0.0001686 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 291.9829° |
| argument of perigee: | 268.4140° |
| revolutions per day: | 15.27574807 |
| mean anomaly at epoch: | 91.6518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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