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 58432U 22151AJA 24358.29194214 .00002016 00000-0 93890-3 0 9998
2 58432 98.8245 11.9596 0013515 105.6556 254.6113 14.21602371 84397
| Epoch (UTC): | 23 December 2024 07:00:23 |
| Eccentricity: | 0.0013515 |
| inclination: | 98.8245° |
| perigee height: | 810 km |
| apogee height: | 829 km |
| right ascension of ascending node: | 11.9596° |
| argument of perigee: | 105.6556° |
| revolutions per day: | 14.21602371 |
| mean anomaly at epoch: | 254.6113° |
| orbit number at epoch: | 8439 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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