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 58082U 26145.59692567 +.00000000 +00000-0 +13571-3 0 00003
2 58082 43.0038 3.9056 0001777 245.6637 114.4029 15.27574763 09
| Epoch (UTC): | 25 May 2026 14:19:34 |
| Eccentricity: | 0.0001777 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 3.9056° |
| argument of perigee: | 245.6637° |
| revolutions per day: | 15.27574763 |
| mean anomaly at epoch: | 114.4029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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