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 37368U 11007A 11172.68686343 .00026098 00000-0 25865-3 0 9996
2 37368 051.6372 138.0216 0019008 277.0049 074.9488 15.65407610 19657
| Epoch (UTC): | 21 June 2011 16:29:05 |
| Eccentricity: | 0.0019008 |
| inclination: | 51.6372° |
| perigee height: | 359 km |
| apogee height: | 385 km |
| right ascension of ascending node: | 138.0216° |
| argument of perigee: | 277.0049° |
| revolutions per day: | 15.65407610 |
| mean anomaly at epoch: | 74.9488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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