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 35690U 09038B 10076.22711312 .05715194 12509-4 31481-3 0 9999
2 35690 051.6170 315.4586 0004999 310.9891 057.3269 16.42150010 36561
| Epoch (UTC): | 17 March 2010 05:27:02 |
| Eccentricity: | 0.0004999 |
| inclination: | 51.6170° |
| perigee height: | 157 km |
| apogee height: | 163 km |
| right ascension of ascending node: | 315.4586° |
| argument of perigee: | 310.9891° |
| revolutions per day: | 16.42150010 |
| mean anomaly at epoch: | 57.3269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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