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 38075U 12005A 12092.56025921 .09065691 11988-4 31544-3 0 9992
2 38075 055.9981 117.2615 0012262 286.1171 073.9276 16.43319523 9352
| Epoch (UTC): | 01 April 2012 13:26:46 |
| Eccentricity: | 0.0012262 |
| inclination: | 55.9981° |
| perigee height: | 149 km |
| apogee height: | 165 km |
| right ascension of ascending node: | 117.2615° |
| argument of perigee: | 286.1171° |
| revolutions per day: | 16.43319523 |
| mean anomaly at epoch: | 73.9276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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