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 26064.47069534 +.00000000 +00000-0 -12085-4 0 00003
2 19120 71.0130 77.4694 0022514 340.5401 19.4862 14.19615722 03
| Epoch (UTC): | 05 March 2026 11:17:48 |
| Eccentricity: | 0.0022514 |
| inclination: | 71.0130° |
| perigee height: | 810 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 77.4694° |
| argument of perigee: | 340.5401° |
| revolutions per day: | 14.19615722 |
| mean anomaly at epoch: | 19.4862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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