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 26137.68117922 +.00000000 +00000-0 -48401-4 0 00003
2 19120 71.0146 282.6627 0023679 237.1827 122.7018 14.19625946 02
| Epoch (UTC): | 17 May 2026 16:20:53 |
| Eccentricity: | 0.0023679 |
| inclination: | 71.0146° |
| perigee height: | 810 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 282.6627° |
| argument of perigee: | 237.1827° |
| revolutions per day: | 14.19625946 |
| mean anomaly at epoch: | 122.7018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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