|
View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line
orbital elements,
1 20580U 90037B 10039.31536863 .00000423 00000-0 19571-4 0 5141
2 20580 028.4702 001.1182 0003300 268.1978 091.8283 15.00889866885362
| Epoch (UTC): | 7:34:08 AM, Monday, February 08, 2010 |
| Eccentricity: | 0.0003300 |
| Inclination: | 028.4702° |
| Perigee Height: | 562 km |
| Apogee Height: | 566 km |
| Right Ascension of Ascending Node: | 001.1182° |
| Argument of Perigee: | 268.1978° |
| Revolutions per Day: | 15.00889866 |
| Mean Anomaly at Epoch: | 091.8283° |
| Orbit Number at Epoch: | 88536 |
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.
|
|
|
|
