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 15027.16649286 .00003634 00000-0 54668-3 0 2235
2 19884 026.5308 317.0499 6036390 256.9844 329.9945 04.00192547298477
| Epoch (UTC): | 27 January 2015 03:59:44 |
| Eccentricity: | 0.6036390 |
| inclination: | 26.5308° |
| perigee height: | 264 km |
| apogee height: | 20495 km |
| right ascension of ascending node: | 317.0499° |
| argument of perigee: | 256.9844° |
| revolutions per day: | 4.00192547 |
| mean anomaly at epoch: | 329.9945° |
| orbit number at epoch: | 29847 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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