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 25544U 26139.81053375 +.00000000 +00000-0 +10220-3 0 00004
2 25544 51.6327 80.5761 0007549 76.5627 283.6202 15.49275597 08
| Epoch (UTC): | 19 May 2026 19:27:10 |
| Eccentricity: | 0.0007549 |
| inclination: | 51.6327° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 80.5761° |
| argument of perigee: | 76.5627° |
| revolutions per day: | 15.49275597 |
| mean anomaly at epoch: | 283.6202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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