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 58107U 26145.44260196 +.00000000 +00000-0 -11103-4 0 00005
2 58107 53.1603 155.2884 0001313 85.3756 274.7396 15.34402952 09
| Epoch (UTC): | 25 May 2026 10:37:20 |
| Eccentricity: | 0.0001313 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 155.2884° |
| argument of perigee: | 85.3756° |
| revolutions per day: | 15.34402952 |
| mean anomaly at epoch: | 274.7396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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