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 35004U 09028D 11247.64656856 .16152067 73217-5 10011-2 0 9990
2 35004 040.4403 342.9642 0002956 038.0069 322.2231 16.41039951130139
| Epoch (UTC): | 04 September 2011 15:31:03 |
| Eccentricity: | 0.0002956 |
| inclination: | 40.4403° |
| perigee height: | 161 km |
| apogee height: | 165 km |
| right ascension of ascending node: | 342.9642° |
| argument of perigee: | 38.0069° |
| revolutions per day: | 16.41039951 |
| mean anomaly at epoch: | 322.2231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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