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 39142U 13016A 13117.34900600 .12996567 12577-4 54149-3 0 9992
2 39142 051.6109 280.4904 0006484 322.5779 038.8670 16.43330407 886
| Epoch (UTC): | 27 April 2013 08:22:34 |
| Eccentricity: | 0.0006484 |
| inclination: | 51.6109° |
| perigee height: | 153 km |
| apogee height: | 161 km |
| right ascension of ascending node: | 280.4904° |
| argument of perigee: | 322.5779° |
| revolutions per day: | 16.43330407 |
| mean anomaly at epoch: | 38.8670° |
| orbit number at epoch: | 88 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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