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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 29303U 89039J 10124.24503764 -.00001726 54567-5 00000+0 0 1467
2 29303 064.7865 078.6696 0492342 340.1646 019.0912 14.88852598 63262
| Epoch (UTC): | 5:52:51 AM, Tuesday, May 04, 2010 |
| Eccentricity: | 0.0492342 |
| Inclination: | 064.7865° |
| Perigee Height: | 258 km |
| Apogee Height: | 945 km |
| Right Ascension of Ascending Node: | 078.6696° |
| Argument of Perigee: | 340.1646° |
| Revolutions per Day: | 14.88852598 |
| Mean Anomaly at Epoch: | 019.0912° |
| Orbit Number at Epoch: | 6326 |
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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