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 26066.16179873 +.00000000 +00000-0 -55000-4 0 00003
2 19120 71.0132 73.8932 0022621 338.0300 21.9853 14.19615500 01
| Epoch (UTC): | 07 March 2026 03:52:59 |
| Eccentricity: | 0.0022621 |
| inclination: | 71.0132° |
| perigee height: | 810 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 73.8932° |
| argument of perigee: | 338.0300° |
| revolutions per day: | 14.19615500 |
| mean anomaly at epoch: | 21.9853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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