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 23083.07007961 -.00000052 00000-0 00000+0 0 9994
2 10953 9.5662 308.8752 0002186 121.3961 223.3613 0.99357285116861
Epoch (UTC): | 24 March 2023 01:40:54 |
Eccentricity: | 0.0002186 |
inclination: | 9.5662° |
perigee height: | 36035 km |
apogee height: | 36054 km |
right ascension of ascending node: | 308.8752° |
argument of perigee: | 121.3961° |
revolutions per day: | 0.99357285 |
mean anomaly at epoch: | 223.3613° |
orbit number at epoch: | 11686 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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