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 58367U 26145.38086162 +.00000000 +00000-0 +74863-4 0 00006
2 58367 43.0014 277.7235 0001752 265.5838 94.4814 15.27578472 06
| Epoch (UTC): | 25 May 2026 09:08:26 |
| Eccentricity: | 0.0001752 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.7235° |
| argument of perigee: | 265.5838° |
| revolutions per day: | 15.27578472 |
| mean anomaly at epoch: | 94.4814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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