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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 25994U 99068A 09324.74570481 .00000049 00000-0 20887-4 0 2574
2 25994 098.2156 037.3705 0000507 094.1994 265.9246 14.57109156527956
| Epoch (UTC): | 5:53:49 PM, Friday, November 20, 2009 |
| Eccentricity: | 0.0000507 |
| Inclination: | 098.2156° |
| Perigee Height: | 702 km |
| Apogee Height: | 703 km |
| Right Ascension of Ascending Node: | 037.3705° |
| Argument of Perigee: | 094.1994° |
| Revolutions per Day: | 14.57109156 |
| Mean Anomaly at Epoch: | 265.9246° |
| Orbit Number at Epoch: | 52795 |
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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