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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 25544U 98067A 09324.89652069 .00016157 00000-0 10314-3 0 222
2 25544 051.6460 221.6824 0005808 002.2379 093.4240 15.76541880630649
| Epoch (UTC): | 9:30:59 PM, Friday, November 20, 2009 |
| Eccentricity: | 0.0005808 |
| Inclination: | 051.6460° |
| Perigee Height: | 336 km |
| Apogee Height: | 344 km |
| Right Ascension of Ascending Node: | 221.6824° |
| Argument of Perigee: | 002.2379° |
| Revolutions per Day: | 15.76541880 |
| Mean Anomaly at Epoch: | 093.4240° |
| Orbit Number at Epoch: | 63064 |
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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