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 39381U 13064B 17030.69460700 +.05363117 +71439-5 +69502-3 0 9991
2 39381 040.4713 023.6434 0005356 189.5894 170.4852 16.34649372180843
| Epoch (UTC): | 30 January 2017 16:40:14 |
| Eccentricity: | 0.0005356 |
| inclination: | 40.4713° |
| perigee height: | 176 km |
| apogee height: | 183 km |
| right ascension of ascending node: | 23.6434° |
| argument of perigee: | 189.5894° |
| revolutions per day: | 16.34649372 |
| mean anomaly at epoch: | 170.4852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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