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 30382U 99025ACV 24358.11503729 .00005175 00000-0 20347-2 0 9997
2 30382 98.5353 41.1838 0159443 311.8735 110.1989 14.22950817924867
Epoch (UTC): | 23 December 2024 02:45:39 |
Eccentricity: | 0.0159443 |
inclination: | 98.5353° |
perigee height: | 700 km |
apogee height: | 930 km |
right ascension of ascending node: | 41.1838° |
argument of perigee: | 311.8735° |
revolutions per day: | 14.22950817 |
mean anomaly at epoch: | 110.1989° |
orbit number at epoch: | 92486 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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