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 27846U 03031G 19345.74760986 +.00000030 +00000-0 +33193-4 0 9999
2 27846 098.6832 349.8130 0008756 210.0809 149.9867 14.22243323853319
Epoch (UTC): | 11 December 2019 17:56:33 |
Eccentricity: | 0.0008756 |
inclination: | 98.6832° |
perigee height: | 811 km |
apogee height: | 824 km |
right ascension of ascending node: | 349.8130° |
argument of perigee: | 210.0809° |
revolutions per day: | 14.22243323 |
mean anomaly at epoch: | 149.9867° |
orbit number at epoch: | 85331 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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