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 15593U 85020B 13143.77038566 .00000376 00000-0 42986-4 0 3513
2 15593 082.5388 211.8555 0010429 259.3302 212.9103 14.83340798524080
| Epoch (UTC): | 23 May 2013 18:29:21 |
| Eccentricity: | 0.0010429 |
| inclination: | 82.5388° |
| perigee height: | 611 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 211.8555° |
| argument of perigee: | 259.3302° |
| revolutions per day: | 14.83340798 |
| mean anomaly at epoch: | 212.9103° |
| orbit number at epoch: | 52408 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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