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 13138.10524282 .00000092 00000-0 45048-4 0 3874
2 27386 098.4290 206.9966 0001236 083.1795 276.9539 14.37609622586812
| Epoch (UTC): | 18 May 2013 02:31:32 |
| Eccentricity: | 0.0001236 |
| inclination: | 98.4290° |
| perigee height: | 765 km |
| apogee height: | 767 km |
| right ascension of ascending node: | 206.9966° |
| argument of perigee: | 83.1795° |
| revolutions per day: | 14.37609622 |
| mean anomaly at epoch: | 276.9539° |
| orbit number at epoch: | 58681 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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