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 25544U 98067A 23337.40753170 .00020668 00000-0 36782-3 0 9996
2 25544 51.6412 210.3871 0001391 7.1799 151.4629 15.50104594428039
| Epoch (UTC): | 03 December 2023 09:46:50 |
| Eccentricity: | 0.0001391 |
| inclination: | 51.6412° |
| perigee height: | 415 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 210.3871° |
| argument of perigee: | 7.1799° |
| revolutions per day: | 15.50104594 |
| mean anomaly at epoch: | 151.4629° |
| orbit number at epoch: | 42803 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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