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 37841U 11058D 22178.37081064 .00000330 00000-0 36043-4 0 9993
2 37841 19.9702 194.9721 0012059 92.9586 295.1089 14.10757909552641
Epoch (UTC): | 27 June 2022 08:53:58 |
Eccentricity: | 0.0012059 |
inclination: | 19.9702° |
perigee height: | 848 km |
apogee height: | 865 km |
right ascension of ascending node: | 194.9721° |
argument of perigee: | 92.9586° |
revolutions per day: | 14.10757909 |
mean anomaly at epoch: | 295.1089° |
orbit number at epoch: | 55264 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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