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 58729U 26145.48440015 +.00000000 +00000-0 +40583-4 0 00002
2 58729 43.0017 146.4558 0001224 269.1763 90.8948 15.27587857 07
| Epoch (UTC): | 25 May 2026 11:37:32 |
| Eccentricity: | 0.0001224 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 146.4558° |
| argument of perigee: | 269.1763° |
| revolutions per day: | 15.27587857 |
| mean anomaly at epoch: | 90.8948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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