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 40927U 15051C 18116.75307241 .00008739 00000-0 17440-3 0 9996
2 40927 97.1973 159.2076 0012060 114.2509 339.0429 15.47002897145262
Epoch (UTC): | 26 April 2018 18:04:25 |
Eccentricity: | 0.0012060 |
inclination: | 97.1973° |
perigee height: | 417 km |
apogee height: | 434 km |
right ascension of ascending node: | 159.2076° |
argument of perigee: | 114.2509° |
revolutions per day: | 15.47002897 |
mean anomaly at epoch: | 339.0429° |
orbit number at epoch: | 14526 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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