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 15332U 84105B 23151.92645427 .00000512 00000-0 58419-4 0 9992
2 15332 82.5328 314.7400 0021807 40.4986 73.1443 14.83993839 67925
Epoch (UTC): | 31 May 2023 22:14:05 |
Eccentricity: | 0.0021807 |
inclination: | 82.5328° |
perigee height: | 601 km |
apogee height: | 632 km |
right ascension of ascending node: | 314.7400° |
argument of perigee: | 40.4986° |
revolutions per day: | 14.83993839 |
mean anomaly at epoch: | 73.1443° |
orbit number at epoch: | 6792 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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