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 39385U 13064F 15259.30680142 .08635644 72055-5 10307-2 0 9991
2 39385 40.5011 209.8243 0005909 232.4787 127.8945 16.35400096102772
| Epoch (UTC): | 16 September 2015 07:21:47 |
| Eccentricity: | 0.0005909 |
| inclination: | 40.5011° |
| perigee height: | 174 km |
| apogee height: | 182 km |
| right ascension of ascending node: | 209.8243° |
| argument of perigee: | 232.4787° |
| revolutions per day: | 16.35400096 |
| mean anomaly at epoch: | 127.8945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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