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 58079U 26145.30583735 +.00000000 +00000-0 -68677-5 0 00004
2 58079 43.0048 5.1675 0001007 283.8799 76.1941 15.27576674 06
| Epoch (UTC): | 25 May 2026 07:20:24 |
| Eccentricity: | 0.0001007 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 5.1675° |
| argument of perigee: | 283.8799° |
| revolutions per day: | 15.27576674 |
| mean anomaly at epoch: | 76.1941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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