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 58001U 26145.60460299 +.00000000 +00000-0 -22890-4 0 00007
2 58001 43.0096 352.3228 0001794 267.0606 93.0040 15.27573258 02
| Epoch (UTC): | 25 May 2026 14:30:37 |
| Eccentricity: | 0.0001794 |
| inclination: | 43.0096° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.3228° |
| argument of perigee: | 267.0606° |
| revolutions per day: | 15.27573258 |
| mean anomaly at epoch: | 93.0040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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