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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 09324.10045530 -.00000018 00000-0 14078-4 0 6594
2 26063 100.2250 139.3107 0037003 182.0086 178.0947 14.35877209514328
| Epoch (UTC): | 2:24:39 AM, Friday, November 20, 2009 |
| Eccentricity: | 0.0037003 |
| Inclination: | 100.2250° |
| Perigee Height: | 745 km |
| Apogee Height: | 798 km |
| Right Ascension of Ascending Node: | 139.3107° |
| Argument of Perigee: | 182.0086° |
| Revolutions per Day: | 14.35877209 |
| Mean Anomaly at Epoch: | 178.0947° |
| Orbit Number at Epoch: | 51432 |
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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