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 23332.55396610 .00000370 00000-0 22353-3 0 9991
2 33591 99.0787 20.9433 0014496 137.9588 222.2698 14.12875037762890
| Epoch (UTC): | 28 November 2023 13:17:42 |
| Eccentricity: | 0.0014496 |
| inclination: | 99.0787° |
| perigee height: | 839 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 20.9433° |
| argument of perigee: | 137.9588° |
| revolutions per day: | 14.12875037 |
| mean anomaly at epoch: | 222.2698° |
| orbit number at epoch: | 76289 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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