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 23331.85688867 .00000031 00000-0 76650-4 0 9991
2 44909 82.5227 239.1786 0217639 164.0242 196.7869 12.79724041183091
| Epoch (UTC): | 27 November 2023 20:33:55 |
| Eccentricity: | 0.0217639 |
| inclination: | 82.5227° |
| perigee height: | 1174 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 239.1786° |
| argument of perigee: | 164.0242° |
| revolutions per day: | 12.79724041 |
| mean anomaly at epoch: | 196.7869° |
| orbit number at epoch: | 18309 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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