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 14206.25007068 .00000885 00000-0 48151-4 0 620
2 20580 028.4700 146.8913 0003074 336.0199 141.3453 15.05552570130465
| Epoch (UTC): | 25 July 2014 06:00:06 |
| Eccentricity: | 0.0003074 |
| inclination: | 28.4700° |
| perigee height: | 547 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 146.8913° |
| argument of perigee: | 336.0199° |
| revolutions per day: | 15.05552570 |
| mean anomaly at epoch: | 141.3453° |
| orbit number at epoch: | 13046 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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