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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 26405U 00039B 10039.70024204 .00021966 -11079-5 70082-4 0 1116
2 26405 087.2170 216.9299 0002720 082.4870 277.6716 15.90710673547160
| Epoch (UTC): | 4:48:21 PM, Monday, February 08, 2010 |
| Eccentricity: | 0.0002720 |
| Inclination: | 087.2170° |
| Perigee Height: | 298 km |
| Apogee Height: | 302 km |
| Right Ascension of Ascending Node: | 216.9299° |
| Argument of Perigee: | 082.4870° |
| Revolutions per Day: | 15.90710673 |
| Mean Anomaly at Epoch: | 277.6716° |
| Orbit Number at Epoch: | 54716 |
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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