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 24279.85431884 .00021555 00000-0 17750-2 0 9991
2 32785 97.7683 244.4812 0008384 333.0304 27.0482 14.99070266892119
| Epoch (UTC): | 05 October 2024 20:30:13 |
| Eccentricity: | 0.0008384 |
| inclination: | 97.7683° |
| perigee height: | 564 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 244.4812° |
| argument of perigee: | 333.0304° |
| revolutions per day: | 14.99070266 |
| mean anomaly at epoch: | 27.0482° |
| orbit number at epoch: | 89211 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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