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 39400U 13064W 16143.09732809 .10280108 73207-5 66774-3 0 9990
2 39400 40.4965 142.2962 0002801 117.1246 243.1418 16.40672040139405
| Epoch (UTC): | 22 May 2016 02:20:09 |
| Eccentricity: | 0.0002801 |
| inclination: | 40.4965° |
| perigee height: | 162 km |
| apogee height: | 166 km |
| right ascension of ascending node: | 142.2962° |
| argument of perigee: | 117.1246° |
| revolutions per day: | 16.40672040 |
| mean anomaly at epoch: | 243.1418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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