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 55579U 26145.45593513 +.00000000 +00000-0 +12278-4 0 00001
2 55579 43.0045 291.6271 0001229 274.9248 85.1464 15.27578999 07
| Epoch (UTC): | 25 May 2026 10:56:32 |
| Eccentricity: | 0.0001229 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 291.6271° |
| argument of perigee: | 274.9248° |
| revolutions per day: | 15.27578999 |
| mean anomaly at epoch: | 85.1464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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