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 13169.35559967 .00000020 00000-0 21154-4 0 4811
2 27386 098.4272 237.6488 0001101 090.8854 269.2460 14.37616375591305
| Epoch (UTC): | 18 June 2013 08:32:03 |
| Eccentricity: | 0.0001101 |
| inclination: | 98.4272° |
| perigee height: | 765 km |
| apogee height: | 767 km |
| right ascension of ascending node: | 237.6488° |
| argument of perigee: | 90.8854° |
| revolutions per day: | 14.37616375 |
| mean anomaly at epoch: | 269.2460° |
| orbit number at epoch: | 59130 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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