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 19211U 26088.21245994 +.00000000 +00000-0 +74694-4 0 00001
2 19211 82.5225 80.0727 0020423 344.6692 15.3903 14.85400842 06
| Epoch (UTC): | 29 March 2026 05:05:56 |
| Eccentricity: | 0.0020423 |
| inclination: | 82.5225° |
| perigee height: | 598 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 80.0727° |
| argument of perigee: | 344.6692° |
| revolutions per day: | 14.85400842 |
| mean anomaly at epoch: | 15.3903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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