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 19120U 26159.45401461 +.00000000 +00000-0 +70234-4 0 00004
2 19120 71.0148 236.6245 0022711 206.0530 153.9454 14.19629145 06
| Epoch (UTC): | 08 June 2026 10:53:46 |
| Eccentricity: | 0.0022711 |
| inclination: | 71.0148° |
| perigee height: | 810 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 236.6245° |
| argument of perigee: | 206.0530° |
| revolutions per day: | 14.19629145 |
| mean anomaly at epoch: | 153.9454° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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