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 58408U 26145.54065252 +.00000000 +00000-0 +11131-3 0 00005
2 58408 43.0065 342.2715 0001838 272.8871 87.1771 15.27581947 04
| Epoch (UTC): | 25 May 2026 12:58:32 |
| Eccentricity: | 0.0001838 |
| inclination: | 43.0065° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.2715° |
| argument of perigee: | 272.8871° |
| revolutions per day: | 15.27581947 |
| mean anomaly at epoch: | 87.1771° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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