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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 29651U 06057A 08052.01700749 .00286558 00000-0 31619-3 0 04
2 29651 58.4796 26.1000 0011038 100.0855 260.1493 16.08904727 04
| Epoch (UTC): | 12:24:29 AM, Thursday, February 21, 2008 |
| Eccentricity: | 0.0011038 |
| Inclination: | 58.4796° |
| Perigee Height: | 242 km |
| Apogee Height: | 257 km |
| Right Ascension of Ascending Node: | 26.1000° |
| Argument of Perigee: | 100.0855° |
| Revolutions per Day: | 16.08904727 |
| Mean Anomaly at Epoch: | 260.1493° |
| Orbit Number at Epoch: | 0 |
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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