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 data is extracted from the following two-line orbital elements,
1 32791U 08021J 19343.53606756 .00000351 00000-0 40926-4 0 9995
2 32791 97.5323 341.2507 0013949 24.9642 335.2248 14.90928006630014
| Epoch (UTC): | 09 December 2019 12:51:56 |
| Eccentricity: | 0.0013949 |
| inclination: | 97.5323° |
| perigee height: | 585 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 341.2507° |
| argument of perigee: | 24.9642° |
| revolutions per day: | 14.90928006 |
| mean anomaly at epoch: | 335.2248° |
| orbit number at epoch: | 63001 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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