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 16327U 85113B 13143.16266605 .00000411 00000-0 48149-4 0 404
2 16327 082.5365 040.8220 0019149 202.0179 308.6605 14.82457194481636
| Epoch (UTC): | 23 May 2013 03:54:14 |
| Eccentricity: | 0.0019149 |
| inclination: | 82.5365° |
| perigee height: | 608 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 40.8220° |
| argument of perigee: | 202.0179° |
| revolutions per day: | 14.82457194 |
| mean anomaly at epoch: | 308.6605° |
| orbit number at epoch: | 48163 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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