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 40012U 14033C 23339.82407021 .00003939 00000-0 53932-3 0 9991
2 40012 97.6823 145.7055 0053677 217.5071 142.2390 14.78040505509113
Epoch (UTC): | 05 December 2023 19:46:39 |
Eccentricity: | 0.0053677 |
inclination: | 97.6823° |
perigee height: | 598 km |
apogee height: | 673 km |
right ascension of ascending node: | 145.7055° |
argument of perigee: | 217.5071° |
revolutions per day: | 14.78040505 |
mean anomaly at epoch: | 142.2390° |
orbit number at epoch: | 50911 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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