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 55584U 26145.42652874 +.00000000 +00000-0 +22304-4 0 00001
2 55584 43.0024 292.2661 0001159 259.1046 100.9675 15.27578433 06
| Epoch (UTC): | 25 May 2026 10:14:12 |
| Eccentricity: | 0.0001159 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 292.2661° |
| argument of perigee: | 259.1046° |
| revolutions per day: | 15.27578433 |
| mean anomaly at epoch: | 100.9675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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