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 56119U 26145.49984794 +.00000000 +00000-0 -44112-5 0 00005
2 56119 43.0025 73.5170 0002143 260.9175 99.1434 15.27576428 08
| Epoch (UTC): | 25 May 2026 11:59:46 |
| Eccentricity: | 0.0002143 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 73.5170° |
| argument of perigee: | 260.9175° |
| revolutions per day: | 15.27576428 |
| mean anomaly at epoch: | 99.1434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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