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 39402U 13064Y 15347.43116619 .06398980 72505-5 67494-3 0 9993
2 39402 40.4724 37.7342 0001558 87.9975 279.0768 16.36588348116099
| Epoch (UTC): | 13 December 2015 10:20:52 |
| Eccentricity: | 0.0001558 |
| inclination: | 40.4724° |
| perigee height: | 174 km |
| apogee height: | 176 km |
| right ascension of ascending node: | 37.7342° |
| argument of perigee: | 87.9975° |
| revolutions per day: | 16.36588348 |
| mean anomaly at epoch: | 279.0768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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