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 20547U 90028B 18111.53658145 .00000583 00000-0 22545-4 0 9994
2 20547 94.0956 298.1284 0083496 187.1013 172.9056 15.24177973546144
Epoch (UTC): | 21 April 2018 12:52:40 |
Eccentricity: | 0.0083496 |
inclination: | 94.0956° |
perigee height: | 436 km |
apogee height: | 550 km |
right ascension of ascending node: | 298.1284° |
argument of perigee: | 187.1013° |
revolutions per day: | 15.24177973 |
mean anomaly at epoch: | 172.9056° |
orbit number at epoch: | 54614 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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