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 39370U 13060A 13319.85296673 -.00001668 00000-0 00000+0 0 9996
2 39370 019.4167 122.9551 9306301 288.8779 002.1288 00.25833433 156
| Epoch (UTC): | 15 November 2013 20:28:16 |
| Eccentricity: | 0.9306301 |
| inclination: | 19.4167° |
| perigee height: | 846 km |
| apogee height: | 194674 km |
| right ascension of ascending node: | 122.9551° |
| argument of perigee: | 288.8779° |
| revolutions per day: | 0.25833433 |
| mean anomaly at epoch: | 2.1288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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