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 58441U 26145.54750659 +.00000000 +00000-0 +31603-4 0 00001
2 58441 43.0029 327.1499 0001124 267.7302 92.3420 15.27575239 08
| Epoch (UTC): | 25 May 2026 13:08:24 |
| Eccentricity: | 0.0001124 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.1499° |
| argument of perigee: | 267.7302° |
| revolutions per day: | 15.27575239 |
| mean anomaly at epoch: | 92.3420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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