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 58041U 26145.52150881 +.00000000 +00000-0 +42383-4 0 00003
2 58041 53.1615 81.3534 0001126 94.8703 265.2427 15.30189338 05
| Epoch (UTC): | 25 May 2026 12:30:58 |
| Eccentricity: | 0.0001126 |
| inclination: | 53.1615° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 81.3534° |
| argument of perigee: | 94.8703° |
| revolutions per day: | 15.30189338 |
| mean anomaly at epoch: | 265.2427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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