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 55576U 26144.82058007 +.00000000 +00000-0 -74109-5 0 00005
2 55576 43.0014 269.4664 0001458 260.3624 99.7063 15.27580649 01
| Epoch (UTC): | 24 May 2026 19:41:38 |
| Eccentricity: | 0.0001458 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 269.4664° |
| argument of perigee: | 260.3624° |
| revolutions per day: | 15.27580649 |
| mean anomaly at epoch: | 99.7063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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