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 13167.74008509 .00000891 00000-0 51223-4 0 2634
2 20580 028.4696 275.7628 0003325 350.3355 136.2094 15.03692199 69630
| Epoch (UTC): | 16 June 2013 17:45:43 |
| Eccentricity: | 0.0003325 |
| inclination: | 28.4696° |
| perigee height: | 553 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 275.7628° |
| argument of perigee: | 350.3355° |
| revolutions per day: | 15.03692199 |
| mean anomaly at epoch: | 136.2094° |
| orbit number at epoch: | 6963 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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