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 32686U 08008A 08273.04186473 .00037110 00000-0 19651-3 0 9991
2 32686 051.6395 202.3391 0011327 317.2751 152.9367 15.80097592 32156
| Epoch (UTC): | 29 September 2008 01:00:17 |
| Eccentricity: | 0.0011327 |
| inclination: | 51.6395° |
| perigee height: | 322 km |
| apogee height: | 338 km |
| right ascension of ascending node: | 202.3391° |
| argument of perigee: | 317.2751° |
| revolutions per day: | 15.80097592 |
| mean anomaly at epoch: | 152.9367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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