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 17295U 87003A 22138.82137732 .00005576 00000-0 27686-3 0 9996
2 17295 82.5132 174.7912 0003898 51.0905 309.0676 15.17487299930800
Epoch (UTC): | 18 May 2022 19:42:47 |
Eccentricity: | 0.0003898 |
inclination: | 82.5132° |
perigee height: | 511 km |
apogee height: | 516 km |
right ascension of ascending node: | 174.7912° |
argument of perigee: | 51.0905° |
revolutions per day: | 15.17487299 |
mean anomaly at epoch: | 309.0676° |
orbit number at epoch: | 93080 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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