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 is defined by the following mean orbital elements,
1 38291U 12022A 12261.05744475 .00009313 00000-0 16691-3 0 9990
2 38291 051.6407 024.6209 0016898 069.6842 086.7860 15.50565903 19440
| Epoch (UTC): | 17 September 2012 01:22:43 |
| Eccentricity: | 0.0016898 |
| inclination: | 51.6407° |
| perigee height: | 403 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 24.6209° |
| argument of perigee: | 69.6842° |
| revolutions per day: | 15.50565903 |
| mean anomaly at epoch: | 86.7860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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