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 26088.21659481 +.00000000 +00000-0 +11178-3 0 00007
2 19120 71.0168 27.2567 0023671 306.3782 53.5159 14.19619295 00
| Epoch (UTC): | 29 March 2026 05:11:53 |
| Eccentricity: | 0.0023671 |
| inclination: | 71.0168° |
| perigee height: | 810 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 27.2567° |
| argument of perigee: | 306.3782° |
| revolutions per day: | 14.19619295 |
| mean anomaly at epoch: | 53.5159° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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