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 23728U 95066A 08323.69802823 0.00000600 00000-0 31670-4 0 02
2 23728 97.9290 101.5081 0307000 194.3756 165.6243 14.83044340 09
| Epoch (UTC): | 18 November 2008 16:45:09 |
| Eccentricity: | 0.0307000 |
| inclination: | 97.9290° |
| perigee height: | 405 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 101.5081° |
| argument of perigee: | 194.3756° |
| revolutions per day: | 14.83044340 |
| mean anomaly at epoch: | 165.6243° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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