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 39025U 12071A 14279.13046825 0.00005000 00000-0 87747-5 0 08
2 39025 43.2190 175.4249 0020000 115.1806 244.8188 16.00659470 09
| Epoch (UTC): | 06 October 2014 03:07:52 |
| Eccentricity: | 0.0020000 |
| inclination: | 43.2190° |
| perigee height: | 259 km |
| apogee height: | 286 km |
| right ascension of ascending node: | 175.4249° |
| argument of perigee: | 115.1806° |
| revolutions per day: | 16.00659470 |
| mean anomaly at epoch: | 244.8188° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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