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 23333.39874432 .00000416 00000-0 21227-3 0 9990
2 31114 98.3029 116.5681 0059257 192.1461 167.8291 14.19665663861740
| Epoch (UTC): | 29 November 2023 09:34:11 |
| Eccentricity: | 0.0059257 |
| inclination: | 98.3029° |
| perigee height: | 784 km |
| apogee height: | 869 km |
| right ascension of ascending node: | 116.5681° |
| argument of perigee: | 192.1461° |
| revolutions per day: | 14.19665663 |
| mean anomaly at epoch: | 167.8291° |
| orbit number at epoch: | 86174 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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