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 20559U 26074.46132874 +.00000000 +00000-0 +97222-3 0 00003
2 20559 30.8080 232.1204 4104158 280.5501 36.9237 7.35436011 00
| Epoch (UTC): | 15 March 2026 11:04:18 |
| Eccentricity: | 0.4104158 |
| inclination: | 30.8080° |
| perigee height: | 207 km |
| apogee height: | 9376 km |
| right ascension of ascending node: | 232.1204° |
| argument of perigee: | 280.5501° |
| revolutions per day: | 7.35436011 |
| mean anomaly at epoch: | 36.9237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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