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 14210.81101655 .00001407 00000-0 83495-4 0 658
2 20580 028.4703 116.9038 0003214 022.9203 023.6251 15.05563308131142
| Epoch (UTC): | 29 July 2014 19:27:51 |
| Eccentricity: | 0.0003214 |
| inclination: | 28.4703° |
| perigee height: | 547 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 116.9038° |
| argument of perigee: | 22.9203° |
| revolutions per day: | 15.05563308 |
| mean anomaly at epoch: | 23.6251° |
| orbit number at epoch: | 13114 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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