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 32249U 07043A 07270.52836325 -.00000070 +00000-0 +00000-0 0 9992
2 32249 028.6369 001.0332 3362896 301.3662 050.8261 02.66564887000007
| Epoch (UTC): | 27 September 2007 12:40:50 |
| Eccentricity: | 0.3362896 |
| inclination: | 28.6369° |
| perigee height: | 8205 km |
| apogee height: | 22982 km |
| right ascension of ascending node: | 1.0332° |
| argument of perigee: | 301.3662° |
| revolutions per day: | 2.66564887 |
| mean anomaly at epoch: | 50.8261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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