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 44909U 19096E 25339.27412444 .00000024 00000-0 56456-4 0 9997
2 44909 82.5199 108.5693 0216839 237.6146 120.3809 12.79745798277549
| Epoch (UTC): | 05 December 2025 06:34:44 |
| Eccentricity: | 0.0216839 |
| inclination: | 82.5199° |
| perigee height: | 1175 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 108.5693° |
| argument of perigee: | 237.6146° |
| revolutions per day: | 12.79745798 |
| mean anomaly at epoch: | 120.3809° |
| orbit number at epoch: | 27754 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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