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 44589U 99057TB 24244.73402199 .00002185 00000-0 31889-3 0 9999
2 44589 98.8204 55.1035 0083507 272.6343 86.5306 14.74671646579131
| Epoch (UTC): | 31 August 2024 17:36:59 |
| Eccentricity: | 0.0083507 |
| inclination: | 98.8204° |
| perigee height: | 587 km |
| apogee height: | 705 km |
| right ascension of ascending node: | 55.1035° |
| argument of perigee: | 272.6343° |
| revolutions per day: | 14.74671646 |
| mean anomaly at epoch: | 86.5306° |
| orbit number at epoch: | 57913 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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