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 62083U 24219C 24358.23596608 .00005303 00000-0 75509-3 0 9998
2 62083 97.9495 156.7859 0000328 58.4797 301.6446 14.77235291 4131
| Epoch (UTC): | 23 December 2024 05:39:47 |
| Eccentricity: | 0.0000328 |
| inclination: | 97.9495° |
| perigee height: | 638 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 156.7859° |
| argument of perigee: | 58.4797° |
| revolutions per day: | 14.77235291 |
| mean anomaly at epoch: | 301.6446° |
| orbit number at epoch: | 413 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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