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 58062U 26145.47501951 +.00000000 +00000-0 +74485-4 0 00006
2 58062 43.0021 313.3709 0001320 266.7435 93.3266 15.27578329 06
| Epoch (UTC): | 25 May 2026 11:24:01 |
| Eccentricity: | 0.0001320 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 313.3709° |
| argument of perigee: | 266.7435° |
| revolutions per day: | 15.27578329 |
| mean anomaly at epoch: | 93.3266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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