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 58004U 26145.61230434 +.00000000 +00000-0 +66917-4 0 00004
2 58004 43.0046 352.3800 0001539 257.7937 102.2742 15.27579482 03
| Epoch (UTC): | 25 May 2026 14:41:43 |
| Eccentricity: | 0.0001539 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.3800° |
| argument of perigee: | 257.7937° |
| revolutions per day: | 15.27579482 |
| mean anomaly at epoch: | 102.2742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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