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 33447U 08062A 17126.26444626 -.00001710 +54069-5 +00000-0 0 9997
2 33447 064.9445 043.2724 0801513 230.1423 216.7698 14.81863300061998
| Epoch (UTC): | 06 May 2017 06:20:48 |
| Eccentricity: | 0.0801513 |
| inclination: | 64.9445° |
| perigee height: | 62 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 43.2724° |
| argument of perigee: | 230.1423° |
| revolutions per day: | 14.81863300 |
| mean anomaly at epoch: | 216.7698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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