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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 25544U 98067A 10212.31345537 .00019269 00000-0 15221-3 0 6186
2 25544 051.6462 004.7791 0007652 166.0155 265.6389 15.71380169670416
| Epoch (UTC): | 7:31:23 AM, Saturday, July 31, 2010 |
| Eccentricity: | 0.0007652 |
| Inclination: | 051.6462° |
| Perigee Height: | 350 km |
| Apogee Height: | 360 km |
| Right Ascension of Ascending Node: | 004.7791° |
| Argument of Perigee: | 166.0155° |
| Revolutions per Day: | 15.71380169 |
| Mean Anomaly at Epoch: | 265.6389° |
| Orbit Number at Epoch: | 67041 |
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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