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 33442U 98067BL 09215.54829407 .13008691 12713-4 15349-3 0 9993
2 33442 051.6268 036.9885 0007699 292.6234 072.1768 16.49476607 40751
| Epoch (UTC): | 03 August 2009 13:09:32 |
| Eccentricity: | 0.0007699 |
| inclination: | 51.6268° |
| perigee height: | 136 km |
| apogee height: | 146 km |
| right ascension of ascending node: | 36.9885° |
| argument of perigee: | 292.6234° |
| revolutions per day: | 16.49476607 |
| mean anomaly at epoch: | 72.1768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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