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 58005U 26145.55462742 +.00000000 +00000-0 +34032-4 0 00000
2 58005 43.0077 352.8048 0001559 262.0909 97.9766 15.27577627 02
| Epoch (UTC): | 25 May 2026 13:18:39 |
| Eccentricity: | 0.0001559 |
| inclination: | 43.0077° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.8048° |
| argument of perigee: | 262.0909° |
| revolutions per day: | 15.27577627 |
| mean anomaly at epoch: | 97.9766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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