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 58487U 26144.99105743 +.00000000 +00000-0 +72435-4 0 00005
2 58487 43.0021 352.8949 0001180 276.9226 83.1491 15.27581611 01
| Epoch (UTC): | 24 May 2026 23:47:07 |
| Eccentricity: | 0.0001180 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.8949° |
| argument of perigee: | 276.9226° |
| revolutions per day: | 15.27581611 |
| mean anomaly at epoch: | 83.1491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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