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 14781U 84021B 24357.85047780 .00003404 00000-0 37375-3 0 9995
2 14781 97.7320 321.9268 0008089 162.5262 197.6235 14.88299682176533
| Epoch (UTC): | 22 December 2024 20:24:41 |
| Eccentricity: | 0.0008089 |
| inclination: | 97.7320° |
| perigee height: | 597 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 321.9268° |
| argument of perigee: | 162.5262° |
| revolutions per day: | 14.88299682 |
| mean anomaly at epoch: | 197.6235° |
| orbit number at epoch: | 17653 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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