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 11239U 79003B 18111.82041204 +.00000062 +00000-0 +48026-4 0 9990
2 11239 082.9410 219.4684 0039511 249.9177 222.3719 13.75823939970039
Epoch (UTC): | 21 April 2018 19:41:23 |
Eccentricity: | 0.0039511 |
inclination: | 82.9410° |
perigee height: | 949 km |
apogee height: | 1008 km |
right ascension of ascending node: | 219.4684° |
argument of perigee: | 249.9177° |
revolutions per day: | 13.75823939 |
mean anomaly at epoch: | 222.3719° |
orbit number at epoch: | 97003 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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