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 16326U 85113A 13168.77737303 .00000674 00000-0 44334-4 0 6639
2 16326 082.5171 196.1249 0011459 235.3576 124.6572 15.05893386496900
| Epoch (UTC): | 17 June 2013 18:39:25 |
| Eccentricity: | 0.0011459 |
| inclination: | 82.5171° |
| perigee height: | 541 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 196.1249° |
| argument of perigee: | 235.3576° |
| revolutions per day: | 15.05893386 |
| mean anomaly at epoch: | 124.6572° |
| orbit number at epoch: | 49690 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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