|
View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line
orbital elements,
1 25791U 99035A 09324.45498073 .00000235 00000-0 16493-4 0 5654
2 25791 024.9847 089.9263 0010453 116.5286 243.6317 14.41805928548970
| Epoch (UTC): | 10:55:10 AM, Friday, November 20, 2009 |
| Eccentricity: | 0.0010453 |
| Inclination: | 024.9847° |
| Perigee Height: | 745 km |
| Apogee Height: | 760 km |
| Right Ascension of Ascending Node: | 089.9263° |
| Argument of Perigee: | 116.5286° |
| Revolutions per Day: | 14.41805928 |
| Mean Anomaly at Epoch: | 243.6317° |
| Orbit Number at Epoch: | 54897 |
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.
|
|
|
|
