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 32765U 08017A 15331.67318444 .04350869 -29703-4 91012-3 0 9996
2 32765 12.9936 147.3205 0006618 28.7193 333.2561 16.29614997418738
| Epoch (UTC): | 27 November 2015 16:09:23 |
| Eccentricity: | 0.0006618 |
| inclination: | 12.9936° |
| perigee height: | 189 km |
| apogee height: | 198 km |
| right ascension of ascending node: | 147.3205° |
| argument of perigee: | 28.7193° |
| revolutions per day: | 16.29614997 |
| mean anomaly at epoch: | 333.2561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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