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 58859U 26145.54871834 +.00000000 +00000-0 +17936-4 0 00006
2 58859 43.0016 175.1551 0001348 273.7982 86.2715 15.27576163 02
| Epoch (UTC): | 25 May 2026 13:10:09 |
| Eccentricity: | 0.0001348 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.1551° |
| argument of perigee: | 273.7982° |
| revolutions per day: | 15.27576163 |
| mean anomaly at epoch: | 86.2715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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