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 37936U 11070A 11330.63367477 +.00002150 -67876-5 +00000-0 0 9996
2 37936 028.9200 110.9743 0119700 209.9800 280.8300 16.12596573000008
| Epoch (UTC): | 26 November 2011 15:12:29 |
| Eccentricity: | 0.0119700 |
| inclination: | 28.9200° |
| perigee height: | 160 km |
| apogee height: | 319 km |
| right ascension of ascending node: | 110.9743° |
| argument of perigee: | 209.9800° |
| revolutions per day: | 16.12596573 |
| mean anomaly at epoch: | 280.8300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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