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 14064U 83044A 18116.16090928 .00000320 00000-0 40898-4 0 9994
2 14064 65.0020 36.1027 0120506 279.6819 79.0702 14.94050141770104
Epoch (UTC): | 26 April 2018 03:51:42 |
Eccentricity: | 0.0120506 |
inclination: | 65.0020° |
perigee height: | 501 km |
apogee height: | 669 km |
right ascension of ascending node: | 36.1027° |
argument of perigee: | 279.6819° |
revolutions per day: | 14.94050141 |
mean anomaly at epoch: | 79.0702° |
orbit number at epoch: | 77010 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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