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 11671U 80005A 14216.59500176 .14838416 -12223-5 12758-3 0 6091
2 11671 082.4436 262.1980 0010847 239.2010 121.7391 16.51711581895956
Epoch (UTC): | 04 August 2014 14:16:48 |
Eccentricity: | 0.0010847 |
inclination: | 82.4436° |
perigee height: | 128 km |
apogee height: | 142 km |
right ascension of ascending node: | 262.1980° |
argument of perigee: | 239.2010° |
revolutions per day: | 16.51711581 |
mean anomaly at epoch: | 121.7391° |
orbit number at epoch: | 89595 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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