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 24357.85309535 .00000369 00000-0 22118-3 0 9999
2 33591 99.0234 55.4328 0014622 118.9668 241.2971 14.13236032818010
| Epoch (UTC): | 22 December 2024 20:28:27 |
| Eccentricity: | 0.0014622 |
| inclination: | 99.0234° |
| perigee height: | 838 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 55.4328° |
| argument of perigee: | 118.9668° |
| revolutions per day: | 14.13236032 |
| mean anomaly at epoch: | 241.2971° |
| orbit number at epoch: | 81801 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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