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 27431U 02024B 23333.69486652 .00000133 00000-0 10123-3 0 9992
2 27431 99.0817 5.7079 0015068 339.0852 20.9699 14.09915750108411
| Epoch (UTC): | 29 November 2023 16:40:36 |
| Eccentricity: | 0.0015068 |
| inclination: | 99.0817° |
| perigee height: | 849 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 5.7079° |
| argument of perigee: | 339.0852° |
| revolutions per day: | 14.09915750 |
| mean anomaly at epoch: | 20.9699° |
| orbit number at epoch: | 10841 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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