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 39439U 13066Z 24357.88312315 .00034736 00000-0 19323-2 0 9999
2 39439 97.7315 321.6591 0031314 211.1409 148.7967 15.13152623599272
| Epoch (UTC): | 22 December 2024 21:11:41 |
| Eccentricity: | 0.0031314 |
| inclination: | 97.7315° |
| perigee height: | 505 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 321.6591° |
| argument of perigee: | 211.1409° |
| revolutions per day: | 15.13152623 |
| mean anomaly at epoch: | 148.7967° |
| orbit number at epoch: | 59927 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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