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 31192U 99025BJW 24355.22978167 .00001990 00000-0 68088-3 0 9994
2 31192 98.5221 344.7720 0263711 60.9911 301.7419 14.19584447916680
| Epoch (UTC): | 20 December 2024 05:30:53 |
| Eccentricity: | 0.0263711 |
| inclination: | 98.5221° |
| perigee height: | 637 km |
| apogee height: | 1017 km |
| right ascension of ascending node: | 344.7720° |
| argument of perigee: | 60.9911° |
| revolutions per day: | 14.19584447 |
| mean anomaly at epoch: | 301.7419° |
| orbit number at epoch: | 91668 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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