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 58508U 26145.41711638 +.00000000 +00000-0 +64112-4 0 00006
2 58508 43.0066 37.1176 0001313 287.4621 72.6087 15.27579222 02
| Epoch (UTC): | 25 May 2026 10:00:38 |
| Eccentricity: | 0.0001313 |
| inclination: | 43.0066° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 37.1176° |
| argument of perigee: | 287.4621° |
| revolutions per day: | 15.27579222 |
| mean anomaly at epoch: | 72.6087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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