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 40911U 15049N 22176.49213823 .00005711 00000-0 27012-3 0 9993
2 40911 97.4900 180.4267 0012264 336.6941 174.5388 15.19712173374075
Epoch (UTC): | 25 June 2022 11:48:40 |
Eccentricity: | 0.0012264 |
inclination: | 97.4900° |
perigee height: | 498 km |
apogee height: | 515 km |
right ascension of ascending node: | 180.4267° |
argument of perigee: | 336.6941° |
revolutions per day: | 15.19712173 |
mean anomaly at epoch: | 174.5388° |
orbit number at epoch: | 37407 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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