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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 09324.11325368 +.00000156 +00000-0 +24353-4 0 09166
2 29252 064.5120 216.3108 0013486 183.6538 176.4487 15.03458256184354
| Epoch (UTC): | 2:43:05 AM, Friday, November 20, 2009 |
| Eccentricity: | 0.0013486 |
| Inclination: | 064.5120° |
| Perigee Height: | 547 km |
| Apogee Height: | 565 km |
| Right Ascension of Ascending Node: | 216.3108° |
| Argument of Perigee: | 183.6538° |
| Revolutions per Day: | 15.03458256 |
| Mean Anomaly at Epoch: | 176.4487° |
| Orbit Number at Epoch: | 18435 |
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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