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 19650U 88102B 21055.43253304 -.00000257 00000-0 -10627-3 0 9992
2 19650 70.9992 60.0469 0016699 287.7477 72.1824 14.15799885666545
Epoch (UTC): | 24 February 2021 10:22:50 |
Eccentricity: | 0.0016699 |
inclination: | 70.9992° |
perigee height: | 827 km |
apogee height: | 851 km |
right ascension of ascending node: | 60.0469° |
argument of perigee: | 287.7477° |
revolutions per day: | 14.15799885 |
mean anomaly at epoch: | 72.1824° |
orbit number at epoch: | 66654 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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