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 58008U 26145.58931977 +.00000000 +00000-0 +81497-4 0 00004
2 58008 43.0015 353.0525 0001622 260.0489 100.0180 15.27580576 05
| Epoch (UTC): | 25 May 2026 14:08:37 |
| Eccentricity: | 0.0001622 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 353.0525° |
| argument of perigee: | 260.0489° |
| revolutions per day: | 15.27580576 |
| mean anomaly at epoch: | 100.0180° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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