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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 25544U 98067A 09325.27701509 .00014116 00000-0 90634-4 0 259
2 25544 051.6459 219.7255 0005833 003.7012 092.9173 15.76546258630701
| Epoch (UTC): | 6:38:54 AM, Saturday, November 21, 2009 |
| Eccentricity: | 0.0005833 |
| Inclination: | 051.6459° |
| Perigee Height: | 336 km |
| Apogee Height: | 344 km |
| Right Ascension of Ascending Node: | 219.7255° |
| Argument of Perigee: | 003.7012° |
| Revolutions per Day: | 15.76546258 |
| Mean Anomaly at Epoch: | 092.9173° |
| Orbit Number at Epoch: | 63070 |
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
Please read the updated
FAQ before sending e-mail.
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