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 10953U 78062A 23267.73280675 .00000010 00000-0 00000+0 0 9999
2 10953 9.1597 307.1608 0003077 199.9729 321.4788 0.99362270118695
Epoch (UTC): | 24 September 2023 17:35:14 |
Eccentricity: | 0.0003077 |
inclination: | 9.1597° |
perigee height: | 36030 km |
apogee height: | 36056 km |
right ascension of ascending node: | 307.1608° |
argument of perigee: | 199.9729° |
revolutions per day: | 0.99362270 |
mean anomaly at epoch: | 321.4788° |
orbit number at epoch: | 11869 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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