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 27424U 02022A 13181.46460596 .00000362 00000-0 80320-4 0 6949
2 27424 098.1964 122.6294 0000326 023.5767 336.5972 14.57143564593456
| Epoch (UTC): | 30 June 2013 11:09:01 |
| Eccentricity: | 0.0000326 |
| inclination: | 98.1964° |
| perigee height: | 702 km |
| apogee height: | 702 km |
| right ascension of ascending node: | 122.6294° |
| argument of perigee: | 23.5767° |
| revolutions per day: | 14.57143564 |
| mean anomaly at epoch: | 336.5972° |
| orbit number at epoch: | 59345 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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