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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 27643U 03002B 09324.23817732 -.00000242 00000-0 -19669-4 0 2323
2 27643 094.0219 028.7859 0009848 283.5969 076.4202 14.97323133374314
| Epoch (UTC): | 5:42:59 AM, Friday, November 20, 2009 |
| Eccentricity: | 0.0009848 |
| Inclination: | 094.0219° |
| Perigee Height: | 568 km |
| Apogee Height: | 582 km |
| Right Ascension of Ascending Node: | 028.7859° |
| Argument of Perigee: | 283.5969° |
| Revolutions per Day: | 14.97323133 |
| Mean Anomaly at Epoch: | 076.4202° |
| Orbit Number at Epoch: | 37431 |
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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