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 33577U 89006BV 08262.39809309 .00000196 00000-0 26663-2 0 9998
2 33577 8.4325 67.1901 7136297 191.8428 25.4255 2.28334305 16641
| Epoch (UTC): | 18 September 2008 09:33:15 |
| Eccentricity: | 0.7136297 |
| inclination: | 8.4325° |
| perigee height: | 598 km |
| apogee height: | 35366 km |
| right ascension of ascending node: | 67.1901° |
| argument of perigee: | 191.8428° |
| revolutions per day: | 2.28334305 |
| mean anomaly at epoch: | 25.4255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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