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 58091U 26145.31482713 +.00000000 +00000-0 +10213-3 0 00003
2 58091 43.0050 5.2293 0001393 277.2622 82.8071 15.27582472 01
| Epoch (UTC): | 25 May 2026 07:33:21 |
| Eccentricity: | 0.0001393 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 5.2293° |
| argument of perigee: | 277.2622° |
| revolutions per day: | 15.27582472 |
| mean anomaly at epoch: | 82.8071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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