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 37675U 11025A 11186.99225022 .08700290 12041-4 23946-3 0 9990
2 37675 055.6603 203.5909 0002842 191.0376 169.7832 16.45542230 3333
| Epoch (UTC): | 05 July 2011 23:48:50 |
| Eccentricity: | 0.0002842 |
| inclination: | 55.6603° |
| perigee height: | 149 km |
| apogee height: | 153 km |
| right ascension of ascending node: | 203.5909° |
| argument of perigee: | 191.0376° |
| revolutions per day: | 16.45542230 |
| mean anomaly at epoch: | 169.7832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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