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 56910U 26145.62087284 +.00000000 +00000-0 +21342-4 0 00005
2 56910 43.0050 356.2253 0000907 267.3001 92.7747 15.27580137 01
| Epoch (UTC): | 25 May 2026 14:54:03 |
| Eccentricity: | 0.0000907 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.2253° |
| argument of perigee: | 267.3001° |
| revolutions per day: | 15.27580137 |
| mean anomaly at epoch: | 92.7747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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