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 39265U 13055A 25340.94317460 .00064208 13264-6 86051-3 0 9992
2 39265 80.9255 297.7947 0344471 344.4490 14.6348 15.10775920638495
| Epoch (UTC): | 06 December 2025 22:38:10 |
| Eccentricity: | 0.0344471 |
| inclination: | 80.9255° |
| perigee height: | 296 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 297.7947° |
| argument of perigee: | 344.4490° |
| revolutions per day: | 15.10775920 |
| mean anomaly at epoch: | 14.6348° |
| orbit number at epoch: | 63849 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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