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 28933U 05035C 06250.56263144 .13300754 00000-0 18638-3 0 4012
2 28933 051.6150 101.2534 0006572 313.0977 047.0289 16.48585101 34276
| Epoch (UTC): | 07 September 2006 13:30:11 |
| Eccentricity: | 0.0006572 |
| inclination: | 51.6150° |
| perigee height: | 139 km |
| apogee height: | 147 km |
| right ascension of ascending node: | 101.2534° |
| argument of perigee: | 313.0977° |
| revolutions per day: | 16.48585101 |
| mean anomaly at epoch: | 47.0289° |
| orbit number at epoch: | 3427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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