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 55820U 23029AA 24358.15756554 -.00000028 00000-0 -10928-3 0 9991
2 55820 87.9001 37.2647 0001490 88.0647 272.0653 13.14503541 89035
| Epoch (UTC): | 23 December 2024 03:46:53 |
| Eccentricity: | 0.0001490 |
| inclination: | 87.9001° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 37.2647° |
| argument of perigee: | 88.0647° |
| revolutions per day: | 13.14503541 |
| mean anomaly at epoch: | 272.0653° |
| orbit number at epoch: | 8903 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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