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 33405U 08052A 08304.99924557 -.00001620 00000-0 00000+0 0 9994
2 33405 018.0795 351.8234 9494907 173.1090 116.9936 00.16996926 09
| Epoch (UTC): | 30 October 2008 23:58:54 |
| Eccentricity: | 0.9494907 |
| inclination: | 18.0795° |
| perigee height: | 575 km |
| apogee height: | 261994 km |
| right ascension of ascending node: | 351.8234° |
| argument of perigee: | 173.1090° |
| revolutions per day: | 0.16996926 |
| mean anomaly at epoch: | 116.9936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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