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 40342U 14080E 24255.89181527 .00000838 00000-0 11696-2 0 9999
2 40342 63.3943 186.7395 0320777 7.6626 352.9134 13.44345946478789
| Epoch (UTC): | 11 September 2024 21:24:12 |
| Eccentricity: | 0.0320777 |
| inclination: | 63.3943° |
| perigee height: | 853 km |
| apogee height: | 1333 km |
| right ascension of ascending node: | 186.7395° |
| argument of perigee: | 7.6626° |
| revolutions per day: | 13.44345946 |
| mean anomaly at epoch: | 352.9134° |
| orbit number at epoch: | 47878 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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