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 56904U 26145.62729764 +.00000000 +00000-0 +25907-4 0 00005
2 56904 43.0055 356.2726 0001298 264.4840 95.5863 15.27585181 01
| Epoch (UTC): | 25 May 2026 15:03:18 |
| Eccentricity: | 0.0001298 |
| inclination: | 43.0055° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.2726° |
| argument of perigee: | 264.4840° |
| revolutions per day: | 15.27585181 |
| mean anomaly at epoch: | 95.5863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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