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 56126U 26145.08312491 +.00000000 +00000-0 +11660-4 0 00007
2 56126 43.0045 75.5501 0001173 263.6735 96.3983 15.27576962 03
| Epoch (UTC): | 25 May 2026 01:59:41 |
| Eccentricity: | 0.0001173 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 75.5501° |
| argument of perigee: | 263.6735° |
| revolutions per day: | 15.27576962 |
| mean anomaly at epoch: | 96.3983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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