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 14069.14061502 .00004544 00000-0 30157-3 0 4556
2 20580 028.4712 328.0252 0003141 311.6590 168.9479 15.04871739109781
| Epoch (UTC): | 10 March 2014 03:22:29 |
| Eccentricity: | 0.0003141 |
| inclination: | 28.4712° |
| perigee height: | 550 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 328.0252° |
| argument of perigee: | 311.6590° |
| revolutions per day: | 15.04871739 |
| mean anomaly at epoch: | 168.9479° |
| orbit number at epoch: | 10978 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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