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 20580U 90037B 13143.97223197 .00002064 00000-0 13507-3 0 2462
2 20580 028.4708 071.5743 0003411 091.2877 001.9491 15.03620150 66049
| Epoch (UTC): | 23 May 2013 23:20:00 |
| Eccentricity: | 0.0003411 |
| inclination: | 28.4708° |
| perigee height: | 553 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 71.5743° |
| argument of perigee: | 91.2877° |
| revolutions per day: | 15.03620150 |
| mean anomaly at epoch: | 1.9491° |
| orbit number at epoch: | 6604 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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