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 58189U 26145.48610462 +.00000000 +00000-0 +69109-4 0 00002
2 58189 43.0028 69.3866 0001166 256.6180 103.4542 15.27582779 02
| Epoch (UTC): | 25 May 2026 11:39:59 |
| Eccentricity: | 0.0001166 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.3866° |
| argument of perigee: | 256.6180° |
| revolutions per day: | 15.27582779 |
| mean anomaly at epoch: | 103.4542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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