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 26432U 99057KD 24357.21131808 .00025648 00000-0 40938-2 0 9993
2 26432 98.5426 91.4409 0088279 96.6421 264.4841 14.69250376291466
| Epoch (UTC): | 22 December 2024 05:04:17 |
| Eccentricity: | 0.0088279 |
| inclination: | 98.5426° |
| perigee height: | 601 km |
| apogee height: | 725 km |
| right ascension of ascending node: | 91.4409° |
| argument of perigee: | 96.6421° |
| revolutions per day: | 14.69250376 |
| mean anomaly at epoch: | 264.4841° |
| orbit number at epoch: | 29146 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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