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 56019U 26145.50866111 +.00000000 +00000-0 +28308-6 0 00007
2 56019 43.0049 331.4236 0001955 278.6018 81.4612 15.27575388 00
| Epoch (UTC): | 25 May 2026 12:12:28 |
| Eccentricity: | 0.0001955 |
| inclination: | 43.0049° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.4236° |
| argument of perigee: | 278.6018° |
| revolutions per day: | 15.27575388 |
| mean anomaly at epoch: | 81.4612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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