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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 29252U 06029A 10040.32891084 .00000124 00000-0 21827-4 0 9774
2 29252 064.5139 316.5177 0002533 130.5451 229.5902 15.03509862196567
| Epoch (UTC): | 7:53:38 AM, Tuesday, February 09, 2010 |
| Eccentricity: | 0.0002533 |
| Inclination: | 064.5139° |
| Perigee Height: | 554 km |
| Apogee Height: | 558 km |
| Right Ascension of Ascending Node: | 316.5177° |
| Argument of Perigee: | 130.5451° |
| Revolutions per Day: | 15.03509862 |
| Mean Anomaly at Epoch: | 229.5902° |
| Orbit Number at Epoch: | 19656 |
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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FAQ before sending e-mail.
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