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 18959U 88020B 13138.18504201 .00000382 00000-0 44549-4 0 9361
2 18959 082.5394 223.2902 0017033 017.5608 044.6904 14.82481948359605
| Epoch (UTC): | 18 May 2013 04:26:27 |
| Eccentricity: | 0.0017033 |
| inclination: | 82.5394° |
| perigee height: | 609 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 223.2902° |
| argument of perigee: | 17.5608° |
| revolutions per day: | 14.82481948 |
| mean anomaly at epoch: | 44.6904° |
| orbit number at epoch: | 35960 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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