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 55824U 23029AE 24358.13645713 -.00000023 00000-0 -88519-4 0 9994
2 55824 87.9255 22.1349 0002005 78.7868 281.3490 13.20769384 90418
| Epoch (UTC): | 23 December 2024 03:16:29 |
| Eccentricity: | 0.0002005 |
| inclination: | 87.9255° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 22.1349° |
| argument of perigee: | 78.7868° |
| revolutions per day: | 13.20769384 |
| mean anomaly at epoch: | 281.3490° |
| orbit number at epoch: | 9041 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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