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 32788U 08021F 22135.89310791 .00006514 00000-0 56759-3 0 9991
2 32788 97.5310 122.3703 0010015 225.5512 134.4891 14.97175831763565
Epoch (UTC): | 15 May 2022 21:26:04 |
Eccentricity: | 0.0010015 |
inclination: | 97.5310° |
perigee height: | 568 km |
apogee height: | 582 km |
right ascension of ascending node: | 122.3703° |
argument of perigee: | 225.5512° |
revolutions per day: | 14.97175831 |
mean anomaly at epoch: | 134.4891° |
orbit number at epoch: | 76356 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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