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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 33442U 98067BL 09215.54829407 .13008691 12713-4 15349-3 0 3986
2 33442 051.6268 036.9885 0007699 292.6234 072.1768 16.49476607 40751
| Epoch (UTC): | 1:09:33 PM, Monday, August 03, 2009 |
| Eccentricity: | 0.0007699 |
| Inclination: | 051.6268° |
| Perigee Height: | 136 km |
| Apogee Height: | 146 km |
| Right Ascension of Ascending Node: | 036.9885° |
| Argument of Perigee: | 292.6234° |
| Revolutions per Day: | 16.49476607 |
| Mean Anomaly at Epoch: | 072.1768° |
| Orbit Number at Epoch: | 4075 |
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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