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 31114U 07010B 24348.59788375 .00000323 00000-0 16763-3 0 9995
2 31114 98.3568 114.4749 0059560 165.2568 195.0363 14.19997396915706
| Epoch (UTC): | 13 December 2024 14:20:57 |
| Eccentricity: | 0.0059560 |
| inclination: | 98.3568° |
| perigee height: | 782 km |
| apogee height: | 868 km |
| right ascension of ascending node: | 114.4749° |
| argument of perigee: | 165.2568° |
| revolutions per day: | 14.19997396 |
| mean anomaly at epoch: | 195.0363° |
| orbit number at epoch: | 91570 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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