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 38082U 12006F 14243.34478676 .13583328 43697-5 37939-3 0 9990
2 38082 069.3815 097.0364 0033293 225.1799 135.4582 16.41261006136239
| Epoch (UTC): | 31 August 2014 08:16:29 |
| Eccentricity: | 0.0033293 |
| inclination: | 69.3815° |
| perigee height: | 140 km |
| apogee height: | 184 km |
| right ascension of ascending node: | 97.0364° |
| argument of perigee: | 225.1799° |
| revolutions per day: | 16.41261006 |
| mean anomaly at epoch: | 135.4582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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