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 58371U 26145.39113429 +.00000000 +00000-0 +23091-3 0 00005
2 58371 43.0007 277.7662 0001680 277.7906 82.2755 15.27583092 01
| Epoch (UTC): | 25 May 2026 09:23:14 |
| Eccentricity: | 0.0001680 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.7662° |
| argument of perigee: | 277.7906° |
| revolutions per day: | 15.27583092 |
| mean anomaly at epoch: | 82.2755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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