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 58011U 26145.60716106 +.00000000 +00000-0 +40362-4 0 00002
2 58011 43.0049 352.3305 0001354 266.8559 93.2137 15.27598548 01
| Epoch (UTC): | 25 May 2026 14:34:18 |
| Eccentricity: | 0.0001354 |
| inclination: | 43.0049° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.3305° |
| argument of perigee: | 266.8559° |
| revolutions per day: | 15.27598548 |
| mean anomaly at epoch: | 93.2137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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