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 39436U 13066W 18138.34627707 .08053685 26553-5 29454-2 0 9995
2 39436 97.7009 274.5525 0018818 286.4398 133.6699 16.24208076248686
| Epoch (UTC): | 18 May 2018 08:18:38 |
| Eccentricity: | 0.0018818 |
| inclination: | 97.7009° |
| perigee height: | 196 km |
| apogee height: | 220 km |
| right ascension of ascending node: | 274.5525° |
| argument of perigee: | 286.4398° |
| revolutions per day: | 16.24208076 |
| mean anomaly at epoch: | 133.6699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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