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 56892U 26145.04810020 +.00000000 +00000-0 +33474-4 0 00001
2 56892 43.0056 17.7815 0001911 264.1246 95.9388 15.27576217 01
| Epoch (UTC): | 25 May 2026 01:09:15 |
| Eccentricity: | 0.0001911 |
| inclination: | 43.0056° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 17.7815° |
| argument of perigee: | 264.1246° |
| revolutions per day: | 15.27576217 |
| mean anomaly at epoch: | 95.9388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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