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 data is extracted from the following two-line orbital elements,
1 14552U 83122B 16269.65784462 .00000101 00000-0 94219-5 0 9991
2 14552 82.5251 324.2659 0016098 315.2020 44.7894 14.83357427769967
| Epoch (UTC): | 25 September 2016 15:47:17 |
| Eccentricity: | 0.0016098 |
| inclination: | 82.5251° |
| perigee height: | 607 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 324.2659° |
| argument of perigee: | 315.2020° |
| revolutions per day: | 14.83357427 |
| mean anomaly at epoch: | 44.7894° |
| orbit number at epoch: | 76996 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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