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 35579U 09037B 10211.27507613 .00000820 00000-0 30766-4 0 2645
2 35579 009.0472 260.5124 0052378 333.5854 026.2039 14.73104996 56286
| Epoch (UTC): | 06:36:06, Friday, July 30, 2010 |
| Eccentricity: | 0.0052378 |
| Inclination: | 9.0472° |
| Perigee height: | 614 km |
| Apogee height: | 688 km |
| Right Ascension of ascending node: | 260.5124° |
| Argument of perigee: | 333.5854° |
| Revolutions per day: | 14.73104996 |
| Mean anomaly at epoch: | 26.2039° |
| Orbit number at epoch: | 5628 |
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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