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 24259.93446636 .00000679 00000-0 38721-3 0 9994
2 33591 99.0384 316.6592 0014306 40.2104 320.0123 14.13119350804183
| Epoch (UTC): | 15 September 2024 22:25:37 |
| Eccentricity: | 0.0014306 |
| inclination: | 99.0384° |
| perigee height: | 838 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 316.6592° |
| argument of perigee: | 40.2104° |
| revolutions per day: | 14.13119350 |
| mean anomaly at epoch: | 320.0123° |
| orbit number at epoch: | 80418 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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