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 26931U 01043C 19342.11813054 -.00000044 00000-0 15056-4 0 9991
2 26931 67.0516 278.7298 0007221 264.6015 95.4263 14.30560916949632
Epoch (UTC): | 08 December 2019 02:50:06 |
Eccentricity: | 0.0007221 |
inclination: | 67.0516° |
perigee height: | 784 km |
apogee height: | 795 km |
right ascension of ascending node: | 278.7298° |
argument of perigee: | 264.6015° |
revolutions per day: | 14.30560916 |
mean anomaly at epoch: | 95.4263° |
orbit number at epoch: | 94963 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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