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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 20580U 90037B 09321.06096865 .00000344 00000-0 13596-4 0 4779
2 20580 028.4692 184.5336 0003392 108.0013 252.0927 15.00854380872848
| Epoch (UTC): | 1:27:48 AM, Tuesday, November 17, 2009 |
| Eccentricity: | 0.0003392 |
| Inclination: | 028.4692° |
| Perigee Height: | 562 km |
| Apogee Height: | 566 km |
| Right Ascension of Ascending Node: | 184.5336° |
| Argument of Perigee: | 108.0013° |
| Revolutions per Day: | 15.00854380 |
| Mean Anomaly at Epoch: | 252.0927° |
| Orbit Number at Epoch: | 87284 |
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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