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 27422U 02021B 19343.20101518 -.00000032 00000-0 37242-5 0 9999
2 27422 98.3246 307.4805 0013393 77.1881 283.0797 14.29279193915951
Epoch (UTC): | 09 December 2019 04:49:27 |
Eccentricity: | 0.0013393 |
inclination: | 98.3246° |
perigee height: | 784 km |
apogee height: | 804 km |
right ascension of ascending node: | 307.4805° |
argument of perigee: | 77.1881° |
revolutions per day: | 14.29279193 |
mean anomaly at epoch: | 283.0797° |
orbit number at epoch: | 91595 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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