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 33441U 08059A 08335.75808271 .00034349 00000-0 24059-3 0 9990
2 33441 051.6445 242.5845 0006407 027.7080 021.7092 15.73864341 2480
| Epoch (UTC): | 30 November 2008 18:11:38 |
| Eccentricity: | 0.0006407 |
| inclination: | 51.6445° |
| perigee height: | 343 km |
| apogee height: | 352 km |
| right ascension of ascending node: | 242.5845° |
| argument of perigee: | 27.7080° |
| revolutions per day: | 15.73864341 |
| mean anomaly at epoch: | 21.7092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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