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 29661U 06055C 07150.05824307 .13324117 12618-4 10400-3 0 9994
2 29661 051.6186 176.5045 0007204 190.7749 188.7342 16.52052832 25544
| Epoch (UTC): | 30 May 2007 01:23:52 |
| Eccentricity: | 0.0007204 |
| inclination: | 51.6186° |
| perigee height: | 129 km |
| apogee height: | 138 km |
| right ascension of ascending node: | 176.5045° |
| argument of perigee: | 190.7749° |
| revolutions per day: | 16.52052832 |
| mean anomaly at epoch: | 188.7342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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