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 32172U 99025CTS 24355.34871170 .00032556 00000-0 21368-2 0 9993
2 32172 99.0786 22.4751 0081848 47.5298 313.2804 15.04816687928119
| Epoch (UTC): | 20 December 2024 08:22:08 |
| Eccentricity: | 0.0081848 |
| inclination: | 99.0786° |
| perigee height: | 495 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 22.4751° |
| argument of perigee: | 47.5298° |
| revolutions per day: | 15.04816687 |
| mean anomaly at epoch: | 313.2804° |
| orbit number at epoch: | 92811 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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