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 58373U 26145.34873238 +.00000000 +00000-0 +76537-4 0 00007
2 58373 43.0029 277.4535 0000853 274.1196 85.9558 15.27577584 06
| Epoch (UTC): | 25 May 2026 08:22:10 |
| Eccentricity: | 0.0000853 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.4535° |
| argument of perigee: | 274.1196° |
| revolutions per day: | 15.27577584 |
| mean anomaly at epoch: | 85.9558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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