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 33386U 08047A 08272.15013951 .00054573 00000-0 29582-3 0 9999
2 33386 042.4044 178.2230 0005368 282.1563 235.6774 15.79173201 410
| Epoch (UTC): | 28 September 2008 03:36:12 |
| Eccentricity: | 0.0005368 |
| inclination: | 42.4044° |
| perigee height: | 329 km |
| apogee height: | 336 km |
| right ascension of ascending node: | 178.2230° |
| argument of perigee: | 282.1563° |
| revolutions per day: | 15.79173201 |
| mean anomaly at epoch: | 235.6774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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