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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): | 4:45:10 PM, Tuesday, November 18, 2008 |
| 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,
and the full part is where it is sunlit.
Developed and maintained by
Chris Peat, Heavens-Above GmbH
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