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 26067.14827608 +.00000000 +00000-0 -47846-4 0 00007
2 19120 71.0132 71.8070 0022697 336.5845 23.4244 14.19615462 00
| Epoch (UTC): | 08 March 2026 03:33:31 |
| Eccentricity: | 0.0022697 |
| inclination: | 71.0132° |
| perigee height: | 810 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 71.8070° |
| argument of perigee: | 336.5845° |
| revolutions per day: | 14.19615462 |
| mean anomaly at epoch: | 23.4244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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