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 is defined by the following mean orbital elements,
1 39246U 13047A 13274.41666670 -.00017976 00000-0 00000+0 0 9992
2 39246 038.6000 228.5760 9598378 157.4930 358.5830 00.10081861 31
| Epoch (UTC): | 01 October 2013 10:00:00 |
| Eccentricity: | 0.9598378 |
| inclination: | 38.6000° |
| perigee height: | 1453 km |
| apogee height: | 375791 km |
| right ascension of ascending node: | 228.5760° |
| argument of perigee: | 157.4930° |
| revolutions per day: | 0.10081861 |
| mean anomaly at epoch: | 358.5830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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