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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   08078.15603191  .00011450  00000-0  44995-4 0   425
2 32686 051.6434 125.6969 0003896 346.8620 110.8544 15.87516491  1420
 
 
| Epoch (UTC):  | 3:44:41 AM, Tuesday, March 18, 2008 |  
| Eccentricity:  | 0.0003896 |  
| Inclination:  | 051.6434° |  
| Perigee Height:  | 306 km |  
| Apogee Height:  | 312 km |  
| Right Ascension of Ascending Node:  | 125.6969° |  
| Argument of Perigee:  | 346.8620° |  
| Revolutions per Day:  | 15.87516491 |  
| Mean Anomaly at Epoch:  | 110.8544° |  
| Orbit Number at Epoch:  | 142 |  
 
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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FAQ before sending e-mail.
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