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 55485U 26145.39504752 +.00000000 +00000-0 +23771-4 0 00007
2 55485 43.0051 266.7737 0002115 275.5016 84.5594 15.27578921 07
| Epoch (UTC): | 25 May 2026 09:28:52 |
| Eccentricity: | 0.0002115 |
| inclination: | 43.0051° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 266.7737° |
| argument of perigee: | 275.5016° |
| revolutions per day: | 15.27578921 |
| mean anomaly at epoch: | 84.5594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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