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 13170.60856412 .00022411 00000-0 14670-2 0 6676
2 19884 026.5038 029.3877 6176920 251.2724 035.3532 03.82698893275467
| Epoch (UTC): | 19 June 2013 14:36:19 |
| Eccentricity: | 0.6176920 |
| inclination: | 26.5038° |
| perigee height: | 222 km |
| apogee height: | 21551 km |
| right ascension of ascending node: | 29.3877° |
| argument of perigee: | 251.2724° |
| revolutions per day: | 3.82698893 |
| mean anomaly at epoch: | 35.3532° |
| orbit number at epoch: | 27546 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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