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 23335.89749398 .00007287 00000-0 99240-3 0 9992
2 40012 97.6824 141.9594 0053508 230.4764 129.1712 14.78002566508538
Epoch (UTC): | 01 December 2023 21:32:23 |
Eccentricity: | 0.0053508 |
inclination: | 97.6824° |
perigee height: | 598 km |
apogee height: | 673 km |
right ascension of ascending node: | 141.9594° |
argument of perigee: | 230.4764° |
revolutions per day: | 14.78002566 |
mean anomaly at epoch: | 129.1712° |
orbit number at epoch: | 50853 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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