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 07714U 75023A 24254.68766308 .00000317 00000-0 17770-3 0 9993
2 07714 81.2067 138.3903 0028043 11.6645 348.5168 14.08311746856810
| Epoch (UTC): | 10 September 2024 16:30:14 |
| Eccentricity: | 0.0028043 |
| inclination: | 81.2067° |
| perigee height: | 845 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 138.3903° |
| argument of perigee: | 11.6645° |
| revolutions per day: | 14.08311746 |
| mean anomaly at epoch: | 348.5168° |
| orbit number at epoch: | 85681 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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