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 17755U 82116D 24357.73321324 .00000075 00000-0 31421-4 0 9996
2 17755 81.2534 196.1568 0069984 97.1188 22.8337 14.14584620168360
| Epoch (UTC): | 22 December 2024 17:35:49 |
| Eccentricity: | 0.0069984 |
| inclination: | 81.2534° |
| perigee height: | 793 km |
| apogee height: | 894 km |
| right ascension of ascending node: | 196.1568° |
| argument of perigee: | 97.1188° |
| revolutions per day: | 14.14584620 |
| mean anomaly at epoch: | 22.8337° |
| orbit number at epoch: | 16836 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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