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 23087.38284351 .00000051 00000-0 15948-3 0 9991
2 44909 82.5235 41.6287 0217932 16.1990 344.5934 12.79719550151826
| Epoch (UTC): | 28 March 2023 09:11:17 |
| Eccentricity: | 0.0217932 |
| inclination: | 82.5235° |
| perigee height: | 1174 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 41.6287° |
| argument of perigee: | 16.1990° |
| revolutions per day: | 12.79719550 |
| mean anomaly at epoch: | 344.5934° |
| orbit number at epoch: | 15182 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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