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 13992U 83031B 24357.51726791 .00000546 00000-0 19237-3 0 9998
2 13992 74.0529 9.8333 0004695 11.9619 348.1645 14.37179212182683
| Epoch (UTC): | 22 December 2024 12:24:51 |
| Eccentricity: | 0.0004695 |
| inclination: | 74.0529° |
| perigee height: | 764 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 9.8333° |
| argument of perigee: | 11.9619° |
| revolutions per day: | 14.37179212 |
| mean anomaly at epoch: | 348.1645° |
| orbit number at epoch: | 18268 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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