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 39684U 14022E 14135.36235261 .07698316 12572-4 48070-3 0 9994
2 39684 051.6249 252.6445 0009352 339.9402 029.7870 16.41029342 4252
| Epoch (UTC): | 15 May 2014 08:41:47 |
| Eccentricity: | 0.0009352 |
| inclination: | 51.6249° |
| perigee height: | 157 km |
| apogee height: | 169 km |
| right ascension of ascending node: | 252.6445° |
| argument of perigee: | 339.9402° |
| revolutions per day: | 16.41029342 |
| mean anomaly at epoch: | 29.7870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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