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 37252U 10066J 10355.60473544 .12256881 92310-6 19975-2 0 9996
2 37252 034.5327 088.4640 0011338 010.1315 351.3122 16.32165367 2078
Epoch (UTC): | 21 December 2010 14:30:49 |
Eccentricity: | 0.0011338 |
inclination: | 34.5327° |
perigee height: | 179 km |
apogee height: | 194 km |
right ascension of ascending node: | 88.4640° |
argument of perigee: | 10.1315° |
revolutions per day: | 16.32165367 |
mean anomaly at epoch: | 351.3122° |
orbit number at epoch: | 207 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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