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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 26626U 00077A 10039.83677011 -.00000148 00000-0 10000-3 0 5479
2 26626 064.2414 013.0292 2667523 270.5945 059.2100 01.00281166 33687
| Epoch (UTC): | 8:04:57 PM, Monday, February 08, 2010 |
| Eccentricity: | 0.2667523 |
| Inclination: | 064.2414° |
| Perigee Height: | 24,537 km |
| Apogee Height: | 47,030 km |
| Right Ascension of Ascending Node: | 013.0292° |
| Argument of Perigee: | 270.5945° |
| Revolutions per Day: | 01.00281166 |
| Mean Anomaly at Epoch: | 059.2100° |
| Orbit Number at Epoch: | 3368 |
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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