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 32785U 08021C 23342.17098393 .00003371 00000-0 32017-3 0 9990
2 32785 97.7296 304.8251 0009974 242.0107 118.0105 14.94139548846850
| Epoch (UTC): | 08 December 2023 04:06:13 |
| Eccentricity: | 0.0009974 |
| inclination: | 97.7296° |
| perigee height: | 578 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 304.8251° |
| argument of perigee: | 242.0107° |
| revolutions per day: | 14.94139548 |
| mean anomaly at epoch: | 118.0105° |
| orbit number at epoch: | 84685 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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