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 27386U 02009A 13138.80124329 .00000126 00000-0 56489-4 0 3890
2 27386 098.4291 207.6794 0001262 082.6172 277.5157 14.37610083586919
| Epoch (UTC): | 18 May 2013 19:13:47 |
| Eccentricity: | 0.0001262 |
| inclination: | 98.4291° |
| perigee height: | 765 km |
| apogee height: | 767 km |
| right ascension of ascending node: | 207.6794° |
| argument of perigee: | 82.6172° |
| revolutions per day: | 14.37610083 |
| mean anomaly at epoch: | 277.5157° |
| orbit number at epoch: | 58691 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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