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 43911U 18112C 24358.17185185 .00000598 00000-0 30029-3 0 9998
2 43911 50.0121 123.2349 0000640 53.8244 306.2731 14.28627438314565
Epoch (UTC): | 23 December 2024 04:07:28 |
Eccentricity: | 0.0000640 |
inclination: | 50.0121° |
perigee height: | 796 km |
apogee height: | 797 km |
right ascension of ascending node: | 123.2349° |
argument of perigee: | 53.8244° |
revolutions per day: | 14.28627438 |
mean anomaly at epoch: | 306.2731° |
orbit number at epoch: | 31456 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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