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 31068U 99025BFN 24352.71593725 .00000799 00000-0 42876-3 0 9993
2 31068 98.5979 344.5781 0166746 60.5268 301.2422 14.08716735912857
| Epoch (UTC): | 17 December 2024 17:10:56 |
| Eccentricity: | 0.0166746 |
| inclination: | 98.5979° |
| perigee height: | 743 km |
| apogee height: | 984 km |
| right ascension of ascending node: | 344.5781° |
| argument of perigee: | 60.5268° |
| revolutions per day: | 14.08716735 |
| mean anomaly at epoch: | 301.2422° |
| orbit number at epoch: | 91285 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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