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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 26063U 00004C 10039.72200228 -.00000027 00000-0 11121-4 0 7232
2 26063 100.2272 234.8226 0036623 316.0482 043.7792 14.35883905525891
| Epoch (UTC): | 5:19:41 PM, Monday, February 08, 2010 |
| Eccentricity: | 0.0036623 |
| Inclination: | 100.2272° |
| Perigee Height: | 746 km |
| Apogee Height: | 798 km |
| Right Ascension of Ascending Node: | 234.8226° |
| Argument of Perigee: | 316.0482° |
| Revolutions per Day: | 14.35883905 |
| Mean Anomaly at Epoch: | 043.7792° |
| Orbit Number at Epoch: | 52589 |
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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