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 32331U 99025CXY 23339.93355007 .00008308 00000-0 31848-2 0 9994
2 32331 99.1986 232.5527 0030476 158.4415 201.8057 14.30547420499432
Epoch (UTC): | 05 December 2023 22:24:18 |
Eccentricity: | 0.0030476 |
inclination: | 99.1986° |
perigee height: | 768 km |
apogee height: | 812 km |
right ascension of ascending node: | 232.5527° |
argument of perigee: | 158.4415° |
revolutions per day: | 14.30547420 |
mean anomaly at epoch: | 201.8057° |
orbit number at epoch: | 49943 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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