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 26064.11838220 +.00000000 +00000-0 -48947-5 0 00007
2 19120 71.0130 78.2145 0022501 341.0700 18.9586 14.19615694 02
| Epoch (UTC): | 05 March 2026 02:50:28 |
| Eccentricity: | 0.0022501 |
| inclination: | 71.0130° |
| perigee height: | 810 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 78.2145° |
| argument of perigee: | 341.0700° |
| revolutions per day: | 14.19615694 |
| mean anomaly at epoch: | 18.9586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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