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 38051U 11062C 14288.65876392 .70201582 12497-4 27925-2 0 9995
2 38051 051.5964 324.1908 0006422 269.6897 186.8903 16.43533377153081
| Epoch (UTC): | 15 October 2014 15:48:37 |
| Eccentricity: | 0.0006422 |
| inclination: | 51.5964° |
| perigee height: | 152 km |
| apogee height: | 160 km |
| right ascension of ascending node: | 324.1908° |
| argument of perigee: | 269.6897° |
| revolutions per day: | 16.43533377 |
| mean anomaly at epoch: | 186.8903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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