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 24357.44941097 .00000024 00000-0 57118-4 0 9992
2 44909 82.5218 339.6723 0216981 331.3277 27.6030 12.79737137233058
| Epoch (UTC): | 22 December 2024 10:47:09 |
| Eccentricity: | 0.0216981 |
| inclination: | 82.5218° |
| perigee height: | 1175 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 339.6723° |
| argument of perigee: | 331.3277° |
| revolutions per day: | 12.79737137 |
| mean anomaly at epoch: | 27.6030° |
| orbit number at epoch: | 23305 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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