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 19884U 89021C 14208.26364762 .00015009 00000-0 14498-2 0 434
2 19884 026.4347 095.0963 6080713 025.4249 158.9093 03.95547427291138
| Epoch (UTC): | 27 July 2014 06:19:39 |
| Eccentricity: | 0.6080713 |
| inclination: | 26.4347° |
| perigee height: | 241 km |
| apogee height: | 20780 km |
| right ascension of ascending node: | 95.0963° |
| argument of perigee: | 25.4249° |
| revolutions per day: | 3.95547427 |
| mean anomaly at epoch: | 158.9093° |
| orbit number at epoch: | 29113 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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