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 39440U 13066AA 25343.11749727 .00007171 00000-0 69180-3 0 9994
2 39440 97.8706 286.7933 0058337 298.0948 61.4381 14.91905889648637
| Epoch (UTC): | 09 December 2025 02:49:11 |
| Eccentricity: | 0.0058337 |
| inclination: | 97.8706° |
| perigee height: | 551 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 286.7933° |
| argument of perigee: | 298.0948° |
| revolutions per day: | 14.91905889 |
| mean anomaly at epoch: | 61.4381° |
| orbit number at epoch: | 64863 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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