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 57924U 26145.56943578 +.00000000 +00000-0 +12438-3 0 00006
2 57924 43.0025 254.5978 0001843 263.9467 96.1175 15.27586064 09
| Epoch (UTC): | 25 May 2026 13:39:59 |
| Eccentricity: | 0.0001843 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 254.5978° |
| argument of perigee: | 263.9467° |
| revolutions per day: | 15.27586064 |
| mean anomaly at epoch: | 96.1175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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