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 19460U 88078A 13160.70205451 0.00000160 00000-0 58496-4 0 02
2 19460 84.9866 354.2212 0003168 227.7268 132.2730 14.33047726 09
| Epoch (UTC): | 09 June 2013 16:50:57 |
| Eccentricity: | 0.0003168 |
| inclination: | 84.9866° |
| perigee height: | 779 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 354.2212° |
| argument of perigee: | 227.7268° |
| revolutions per day: | 14.33047726 |
| mean anomaly at epoch: | 132.2730° |
| 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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