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 39435U 13066V 14099.35188471 .00002386 00000-0 27506-3 0 9992
2 39435 97.7868 174.0379 0056077 109.7041 251.0236 14.85489138 20584
| Epoch (UTC): | 09 April 2014 08:26:42 |
| Eccentricity: | 0.0056077 |
| inclination: | 97.7868° |
| perigee height: | 573 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 174.0379° |
| argument of perigee: | 109.7041° |
| revolutions per day: | 14.85489138 |
| mean anomaly at epoch: | 251.0236° |
| orbit number at epoch: | 2058 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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