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 18362U 87080B 23083.90004227 .00000128 00000-0 19992-3 0 9997
2 18362 90.3443 43.9746 0104740 210.6263 203.4576 13.44195078741577
Epoch (UTC): | 24 March 2023 21:36:03 |
Eccentricity: | 0.0104740 |
inclination: | 90.3443° |
perigee height: | 1015 km |
apogee height: | 1172 km |
right ascension of ascending node: | 43.9746° |
argument of perigee: | 210.6263° |
revolutions per day: | 13.44195078 |
mean anomaly at epoch: | 203.4576° |
orbit number at epoch: | 74157 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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