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 40960U 15057C 23338.10456196 .00001436 00000-0 22168-3 0 9994
2 40960 97.6878 5.6632 0018695 39.0762 321.1794 14.74678884438823
| Epoch (UTC): | 04 December 2023 02:30:34 |
| Eccentricity: | 0.0018695 |
| inclination: | 97.6878° |
| perigee height: | 633 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 5.6632° |
| argument of perigee: | 39.0762° |
| revolutions per day: | 14.74678884 |
| mean anomaly at epoch: | 321.1794° |
| orbit number at epoch: | 43882 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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