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 11671U 80005A 13338.13825997 .00034104 00000-0 45441-3 0 2795
2 11671 082.4743 167.2942 0004392 354.9698 144.1795 15.57954731857580
| Epoch (UTC): | 04 December 2013 03:19:05 |
| Eccentricity: | 0.0004392 |
| inclination: | 82.4743° |
| perigee height: | 390 km |
| apogee height: | 396 km |
| right ascension of ascending node: | 167.2942° |
| argument of perigee: | 354.9698° |
| revolutions per day: | 15.57954731 |
| mean anomaly at epoch: | 144.1795° |
| orbit number at epoch: | 85758 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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