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 23968U 96042B 24287.34177669 .00003752 00000-0 17156-2 0 9994
2 23968 26.6811 211.2941 6364963 224.9749 61.3683 3.46987938336352
| Epoch (UTC): | 13 October 2024 08:12:09 |
| Eccentricity: | 0.6364963 |
| inclination: | 26.6811° |
| perigee height: | 321 km |
| apogee height: | 23782 km |
| right ascension of ascending node: | 211.2941° |
| argument of perigee: | 224.9749° |
| revolutions per day: | 3.46987938 |
| mean anomaly at epoch: | 61.3683° |
| orbit number at epoch: | 33635 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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