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 35003U 09028C 11278.76493853 +.05638703 +71200-5 +11831-2 0 9997
2 35003 040.4370 161.0594 0006849 275.9761 084.3784 16.29831142134897
| Epoch (UTC): | 05 October 2011 18:21:30 |
| Eccentricity: | 0.0006849 |
| inclination: | 40.4370° |
| perigee height: | 188 km |
| apogee height: | 197 km |
| right ascension of ascending node: | 161.0594° |
| argument of perigee: | 275.9761° |
| revolutions per day: | 16.29831142 |
| mean anomaly at epoch: | 84.3784° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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