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 13168.52483485 .00000203 00000-0 22173-4 0 620
2 16327 082.5340 017.1458 0020901 121.9983 299.8376 14.82470991485392
| Epoch (UTC): | 17 June 2013 12:35:45 |
| Eccentricity: | 0.0020901 |
| inclination: | 82.5340° |
| perigee height: | 607 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 17.1458° |
| argument of perigee: | 121.9983° |
| revolutions per day: | 14.82470991 |
| mean anomaly at epoch: | 299.8376° |
| orbit number at epoch: | 48539 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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