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 33591U 09005A 23335.74072454 .00000408 00000-0 24346-3 0 9998
2 33591 99.0780 24.1729 0014604 129.5385 230.7079 14.12878323763608
| Epoch (UTC): | 01 December 2023 17:46:38 |
| Eccentricity: | 0.0014604 |
| inclination: | 99.0780° |
| perigee height: | 839 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 24.1729° |
| argument of perigee: | 129.5385° |
| revolutions per day: | 14.12878323 |
| mean anomaly at epoch: | 230.7079° |
| orbit number at epoch: | 76360 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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