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 15392U 84115B 18113.90012288 +.00000151 +00000-0 +62079-5 0 9999
2 15392 021.4924 331.3064 1034180 044.5268 323.3737 12.45557078504999
Epoch (UTC): | 23 April 2018 21:36:10 |
Eccentricity: | 0.1034180 |
inclination: | 21.4924° |
perigee height: | 670 km |
apogee height: | 2296 km |
right ascension of ascending node: | 331.3064° |
argument of perigee: | 44.5268° |
revolutions per day: | 12.45557078 |
mean anomaly at epoch: | 323.3737° |
orbit number at epoch: | 50499 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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