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 is defined by the following mean orbital elements,
1 37361U 10062L 11240.08287324 0.00080000 00000-0 34962-2 0 08
2 37361 71.9798 226.5786 0035921 239.3813 120.6187 15.21395592 05
| Epoch (UTC): | 28 August 2011 01:59:20 |
| Eccentricity: | 0.0035921 |
| inclination: | 71.9798° |
| perigee height: | 477 km |
| apogee height: | 526 km |
| right ascension of ascending node: | 226.5786° |
| argument of perigee: | 239.3813° |
| revolutions per day: | 15.21395592 |
| mean anomaly at epoch: | 120.6187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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