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 55572U 26145.45544456 +.00000000 +00000-0 +76257-5 0 00004
2 55572 43.0013 295.0406 0001085 272.4281 87.6446 15.27576234 00
| Epoch (UTC): | 25 May 2026 10:55:50 |
| Eccentricity: | 0.0001085 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 295.0406° |
| argument of perigee: | 272.4281° |
| revolutions per day: | 15.27576234 |
| mean anomaly at epoch: | 87.6446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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