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 00012U 59001B 24316.55380790 .00002222 00000-0 12748-2 0 9993
2 00012 32.9087 116.7464 1652706 262.3719 78.6891 11.47390953464353
Epoch (UTC): | 11 November 2024 13:17:29 |
Eccentricity: | 0.1652706 |
inclination: | 32.9087° |
perigee height: | 553 km |
apogee height: | 3297 km |
right ascension of ascending node: | 116.7464° |
argument of perigee: | 262.3719° |
revolutions per day: | 11.47390953 |
mean anomaly at epoch: | 78.6891° |
orbit number at epoch: | 46435 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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