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 22286U 92094A 23150.94709526 .00001729 00000-0 17575-3 0 9994
2 22286 82.5181 122.3010 0022354 98.2253 262.1502 14.90056049624740
Epoch (UTC): | 30 May 2023 22:43:49 |
Eccentricity: | 0.0022354 |
inclination: | 82.5181° |
perigee height: | 582 km |
apogee height: | 613 km |
right ascension of ascending node: | 122.3010° |
argument of perigee: | 98.2253° |
revolutions per day: | 14.90056049 |
mean anomaly at epoch: | 262.1502° |
orbit number at epoch: | 62474 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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