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 data is extracted from the following two-line orbital elements,
1 29667U 06055J 08146.34060426 .11864717 12752-4 73624-4 0 9992
2 29667 051.6107 065.3702 0009039 260.8350 099.5042 16.53464210 82911
| Epoch (UTC): | 25 May 2008 08:10:28 |
| Eccentricity: | 0.0009039 |
| inclination: | 51.6107° |
| perigee height: | 124 km |
| apogee height: | 136 km |
| right ascension of ascending node: | 65.3702° |
| argument of perigee: | 260.8350° |
| revolutions per day: | 16.53464210 |
| mean anomaly at epoch: | 99.5042° |
| orbit number at epoch: | 8291 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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