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 34808U 09019B 12108.60339928 .08958927 78882-5 11315-2 0 9993
2 34808 041.1803 169.7480 0004560 335.4943 024.6783 16.34916672168621
Epoch (UTC): | 17 April 2012 14:28:53 |
Eccentricity: | 0.0004560 |
inclination: | 41.1803° |
perigee height: | 176 km |
apogee height: | 182 km |
right ascension of ascending node: | 169.7480° |
argument of perigee: | 335.4943° |
revolutions per day: | 16.34916672 |
mean anomaly at epoch: | 24.6783° |
orbit number at epoch: | 16862 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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