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 23342.42012809 .00000159 00000-0 92504-4 0 9997
2 31114 98.3033 125.0325 0059829 165.8689 194.4179 14.19672170863024
| Epoch (UTC): | 08 December 2023 10:04:59 |
| Eccentricity: | 0.0059829 |
| inclination: | 98.3033° |
| perigee height: | 783 km |
| apogee height: | 869 km |
| right ascension of ascending node: | 125.0325° |
| argument of perigee: | 165.8689° |
| revolutions per day: | 14.19672170 |
| mean anomaly at epoch: | 194.4179° |
| orbit number at epoch: | 86302 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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