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 39407U 13064AD 15325.24148774 .05332726 71609-5 97768-3 0 9996
2 39407 40.4465 172.9823 0019250 281.8405 78.1914 16.30649359110711
| Epoch (UTC): | 21 November 2015 05:47:44 |
| Eccentricity: | 0.0019250 |
| inclination: | 40.4465° |
| perigee height: | 178 km |
| apogee height: | 203 km |
| right ascension of ascending node: | 172.9823° |
| argument of perigee: | 281.8405° |
| revolutions per day: | 16.30649359 |
| mean anomaly at epoch: | 78.1914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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