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 14051U 83041B 24357.80774018 .00006755 00000-0 58923-3 0 9996
2 14051 25.3335 219.8384 1014937 236.0382 113.9550 13.27447922939598
Epoch (UTC): | 22 December 2024 19:23:08 |
Eccentricity: | 0.1014937 |
inclination: | 25.3335° |
perigee height: | 392 km |
apogee height: | 1921 km |
right ascension of ascending node: | 219.8384° |
argument of perigee: | 236.0382° |
revolutions per day: | 13.27447922 |
mean anomaly at epoch: | 113.9550° |
orbit number at epoch: | 93959 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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