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 15890U 85058B 22147.67349101 .00000357 00000-0 40233-4 0 9997
2 15890 82.5276 10.8744 0021635 31.0434 329.2054 14.83602501971418
Epoch (UTC): | 27 May 2022 16:09:49 |
Eccentricity: | 0.0021635 |
inclination: | 82.5276° |
perigee height: | 603 km |
apogee height: | 633 km |
right ascension of ascending node: | 10.8744° |
argument of perigee: | 31.0434° |
revolutions per day: | 14.83602501 |
mean anomaly at epoch: | 329.2054° |
orbit number at epoch: | 97141 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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