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 24340.56272653 .00000019 00000-0 30753-4 0 9992
2 44909 82.5216 350.8968 0217679 10.8400 349.7282 12.79736621230897
| Epoch (UTC): | 05 December 2024 13:30:19 |
| Eccentricity: | 0.0217679 |
| inclination: | 82.5216° |
| perigee height: | 1174 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 350.8968° |
| argument of perigee: | 10.8400° |
| revolutions per day: | 12.79736621 |
| mean anomaly at epoch: | 349.7282° |
| orbit number at epoch: | 23089 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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