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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 32686U 08008A 08081.18896693 .00007849 00000-0 52614-4 0 595
2 32686 051.6420 109.9938 0000597 314.6039 122.7315 15.76378986 1902
| Epoch (UTC): | 4:32:07 AM, Friday, March 21, 2008 |
| Eccentricity: | 0.0000597 |
| Inclination: | 051.6420° |
| Perigee Height: | 340 km |
| Apogee Height: | 341 km |
| Right Ascension of Ascending Node: | 109.9938° |
| Argument of Perigee: | 314.6039° |
| Revolutions per Day: | 15.76378986 |
| Mean Anomaly at Epoch: | 122.7315° |
| Orbit Number at Epoch: | 190 |
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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