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 43807U 18099BB 23273.44431874 .00006629 00000-0 52225-3 0 9993
2 43807 97.5663 334.0119 0006936 82.9323 277.2690 15.01089354262887
Epoch (UTC): | 30 September 2023 10:39:49 |
Eccentricity: | 0.0006936 |
inclination: | 97.5663° |
perigee height: | 559 km |
apogee height: | 568 km |
right ascension of ascending node: | 334.0119° |
argument of perigee: | 82.9323° |
revolutions per day: | 15.01089354 |
mean anomaly at epoch: | 277.2690° |
orbit number at epoch: | 26288 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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