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 58629U 26145.28753703 +.00000000 +00000-0 +85181-5 0 00004
2 58629 43.0047 358.1524 0001272 277.3598 82.7109 15.27575695 00
| Epoch (UTC): | 25 May 2026 06:54:03 |
| Eccentricity: | 0.0001272 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 358.1524° |
| argument of perigee: | 277.3598° |
| revolutions per day: | 15.27575695 |
| mean anomaly at epoch: | 82.7109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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