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 24260.81801034 .00000013 00000-0 79314-5 0 9993
2 44909 82.5219 43.8701 0217302 196.7223 162.6636 12.79733951220699
| Epoch (UTC): | 16 September 2024 19:37:56 |
| Eccentricity: | 0.0217302 |
| inclination: | 82.5219° |
| perigee height: | 1175 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 43.8701° |
| argument of perigee: | 196.7223° |
| revolutions per day: | 12.79733951 |
| mean anomaly at epoch: | 162.6636° |
| orbit number at epoch: | 22069 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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