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 54508U 22151JL 23333.59734591 .00044859 00000-0 99528-2 0 9995
2 54508 98.6780 351.0826 0092012 238.6056 120.6115 14.54260171 54940
| Epoch (UTC): | 29 November 2023 14:20:10 |
| Eccentricity: | 0.0092012 |
| inclination: | 98.6780° |
| perigee height: | 646 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 351.0826° |
| argument of perigee: | 238.6056° |
| revolutions per day: | 14.54260171 |
| mean anomaly at epoch: | 120.6115° |
| orbit number at epoch: | 5494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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