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 26067.00735073 +.00000000 +00000-0 -48698-4 0 00002
2 19120 71.0132 72.1050 0022689 336.7891 23.2208 14.19615475 08
| Epoch (UTC): | 08 March 2026 00:10:35 |
| Eccentricity: | 0.0022689 |
| inclination: | 71.0132° |
| perigee height: | 810 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 72.1050° |
| argument of perigee: | 336.7891° |
| revolutions per day: | 14.19615475 |
| mean anomaly at epoch: | 23.2208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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