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 58682U 26145.34973198 +.00000000 +00000-0 +19612-3 0 00006
2 58682 43.0056 11.9181 0001434 262.0744 97.9945 15.27611687 04
| Epoch (UTC): | 25 May 2026 08:23:36 |
| Eccentricity: | 0.0001434 |
| inclination: | 43.0056° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 11.9181° |
| argument of perigee: | 262.0744° |
| revolutions per day: | 15.27611687 |
| mean anomaly at epoch: | 97.9945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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