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 39932U 94029AGF 24351.30971427 .00005281 00000-0 13034-2 0 9997
2 39932 81.8190 6.7311 0306219 299.6426 57.4578 14.27327657101622
| Epoch (UTC): | 16 December 2024 07:25:59 |
| Eccentricity: | 0.0306219 |
| inclination: | 81.8190° |
| perigee height: | 581 km |
| apogee height: | 1020 km |
| right ascension of ascending node: | 6.7311° |
| argument of perigee: | 299.6426° |
| revolutions per day: | 14.27327657 |
| mean anomaly at epoch: | 57.4578° |
| orbit number at epoch: | 10162 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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