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 56109U 26144.96468860 +.00000000 +00000-0 +21152-5 0 00004
2 56109 43.0053 91.0543 0001297 284.3415 75.7292 15.27573392 02
| Epoch (UTC): | 24 May 2026 23:09:09 |
| Eccentricity: | 0.0001297 |
| inclination: | 43.0053° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 91.0543° |
| argument of perigee: | 284.3415° |
| revolutions per day: | 15.27573392 |
| mean anomaly at epoch: | 75.7292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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