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 20638U 90049A 11295.95477602 +.11801250 +12635-4 +14055-3 0 9996
2 20638 052.9649 145.0450 0003875 266.7349 093.8309 16.49742883194609
Epoch (UTC): | 22 October 2011 22:54:52 |
Eccentricity: | 0.0003875 |
inclination: | 52.9649° |
perigee height: | 137 km |
apogee height: | 142 km |
right ascension of ascending node: | 145.0450° |
argument of perigee: | 266.7349° |
revolutions per day: | 16.49742883 |
mean anomaly at epoch: | 93.8309° |
orbit number at epoch: | 19460 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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