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 43803U 18099AX 24260.70118334 .00019608 00000-0 11987-2 0 9998
2 43803 97.5114 317.4462 0008583 356.8065 3.3108 15.10262602316494
Epoch (UTC): | 16 September 2024 16:49:42 |
Eccentricity: | 0.0008583 |
inclination: | 97.5114° |
perigee height: | 529 km |
apogee height: | 541 km |
right ascension of ascending node: | 317.4462° |
argument of perigee: | 356.8065° |
revolutions per day: | 15.10262602 |
mean anomaly at epoch: | 3.3108° |
orbit number at epoch: | 31649 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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