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 42759U 17034B 22146.97143916 .00005603 00000-0 33522-3 0 9999
2 42759 43.0169 91.0963 0007828 162.9178 279.3829 15.11765024273104
Epoch (UTC): | 26 May 2022 23:18:52 |
Eccentricity: | 0.0007828 |
inclination: | 43.0169° |
perigee height: | 525 km |
apogee height: | 536 km |
right ascension of ascending node: | 91.0963° |
argument of perigee: | 162.9178° |
revolutions per day: | 15.11765024 |
mean anomaly at epoch: | 279.3829° |
orbit number at epoch: | 27310 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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