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 22220U 92076B 13140.13871705 .00000044 00000-0 46320-4 0 407
2 22220 071.0007 313.2381 0012406 012.1244 109.5032 14.16257441 59934
| Epoch (UTC): | 20 May 2013 03:19:45 |
| Eccentricity: | 0.0012406 |
| inclination: | 71.0007° |
| perigee height: | 829 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 313.2381° |
| argument of perigee: | 12.1244° |
| revolutions per day: | 14.16257441 |
| mean anomaly at epoch: | 109.5032° |
| orbit number at epoch: | 5993 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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