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 38096U 12010A 12276.81682870 .00016007 00000-0 26015-3 0 9999
2 38096 051.6482 306.4634 0007858 138.3310 215.8345 15.52835200 30144
Epoch (UTC): | 02 October 2012 19:36:14 |
Eccentricity: | 0.0007858 |
inclination: | 51.6482° |
perigee height: | 403 km |
apogee height: | 414 km |
right ascension of ascending node: | 306.4634° |
argument of perigee: | 138.3310° |
revolutions per day: | 15.52835200 |
mean anomaly at epoch: | 215.8345° |
orbit number at epoch: | 3014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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