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 58590U 26145.26711131 +.00000000 +00000-0 -46693-4 0 00003
2 58590 43.0056 99.6834 0001887 251.4543 108.6104 15.27554888 07
| Epoch (UTC): | 25 May 2026 06:24:38 |
| Eccentricity: | 0.0001887 |
| inclination: | 43.0056° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 99.6834° |
| argument of perigee: | 251.4543° |
| revolutions per day: | 15.27554888 |
| mean anomaly at epoch: | 108.6104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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