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 23335.47389357 .00007535 00000-0 70986-3 0 9991
2 32785 97.7307 298.2337 0009722 269.0219 90.9887 14.94069608845851
| Epoch (UTC): | 01 December 2023 11:22:24 |
| Eccentricity: | 0.0009722 |
| inclination: | 97.7307° |
| perigee height: | 578 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 298.2337° |
| argument of perigee: | 269.0219° |
| revolutions per day: | 14.94069608 |
| mean anomaly at epoch: | 90.9887° |
| orbit number at epoch: | 84585 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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