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 40078U 14037K 24279.89711112 .00002810 00000-0 59993-3 0 9997
2 40078 98.0069 270.2788 0132975 191.2313 168.5910 14.54215015543060
| Epoch (UTC): | 05 October 2024 21:31:50 |
| Eccentricity: | 0.0132975 |
| inclination: | 98.0069° |
| perigee height: | 617 km |
| apogee height: | 806 km |
| right ascension of ascending node: | 270.2788° |
| argument of perigee: | 191.2313° |
| revolutions per day: | 14.54215015 |
| mean anomaly at epoch: | 168.5910° |
| orbit number at epoch: | 54306 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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