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 05678U 71110A 14246.05611296 0.00000067 00000-0 71411-4 0 07
2 05678 69.9760 257.1462 0007000 189.3896 170.6103 13.73911638 03
| Epoch (UTC): | 03 September 2014 01:20:48 |
| Eccentricity: | 0.0007000 |
| inclination: | 69.9760° |
| perigee height: | 980 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 257.1462° |
| argument of perigee: | 189.3896° |
| revolutions per day: | 13.73911638 |
| mean anomaly at epoch: | 170.6103° |
| 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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