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 13168.15552992 .00000246 00000-0 64657-4 0 6937
2 27424 098.1994 109.5348 0001012 098.0443 328.0065 14.57134836591510
| Epoch (UTC): | 17 June 2013 03:43:57 |
| Eccentricity: | 0.0001012 |
| inclination: | 98.1994° |
| perigee height: | 702 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 109.5348° |
| argument of perigee: | 98.0443° |
| revolutions per day: | 14.57134836 |
| mean anomaly at epoch: | 328.0065° |
| orbit number at epoch: | 59151 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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