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 38037U 11078B 11358.49032868 .12429261 12486-4 31801-3 0 9994
2 38037 051.6250 282.3996 0011447 105.0465 255.1538 16.44922867 489
Epoch (UTC): | 24 December 2011 11:46:04 |
Eccentricity: | 0.0011447 |
inclination: | 51.6250° |
perigee height: | 145 km |
apogee height: | 160 km |
right ascension of ascending node: | 282.3996° |
argument of perigee: | 105.0465° |
revolutions per day: | 16.44922867 |
mean anomaly at epoch: | 255.1538° |
orbit number at epoch: | 48 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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