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 39146U 13016E 13116.54817282 .10408996 12279-4 81006-3 0 9993
2 39146 051.6222 284.8782 0010197 234.3737 126.2083 16.39220554 660
| Epoch (UTC): | 26 April 2013 13:09:22 |
| Eccentricity: | 0.0010197 |
| inclination: | 51.6222° |
| perigee height: | 161 km |
| apogee height: | 174 km |
| right ascension of ascending node: | 284.8782° |
| argument of perigee: | 234.3737° |
| revolutions per day: | 16.39220554 |
| mean anomaly at epoch: | 126.2083° |
| orbit number at epoch: | 66 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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