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 58359U 26145.42391735 +.00000000 +00000-0 +12614-3 0 00002
2 58359 43.0027 280.5921 0001411 290.3002 69.7698 15.27583626 08
| Epoch (UTC): | 25 May 2026 10:10:26 |
| Eccentricity: | 0.0001411 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 280.5921° |
| argument of perigee: | 290.3002° |
| revolutions per day: | 15.27583626 |
| mean anomaly at epoch: | 69.7698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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