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 34808U 09019B 12108.60339928 .08958927 78882-5 11315-2 0 9993
2 34808 041.1803 169.7480 0004560 335.4943 024.6783 16.34916672168621
| Epoch (UTC): | 17 April 2012 14:28:53 |
| Eccentricity: | 0.0004560 |
| inclination: | 41.1803° |
| perigee height: | 176 km |
| apogee height: | 182 km |
| right ascension of ascending node: | 169.7480° |
| argument of perigee: | 335.4943° |
| revolutions per day: | 16.34916672 |
| mean anomaly at epoch: | 24.6783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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