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 15063.66761795 .00005471 00000-0 81745-3 0 9997
2 19884 026.4847 289.5846 6033662 303.0284 020.8793 04.00559271299935
| Epoch (UTC): | 04 March 2015 16:01:22 |
| Eccentricity: | 0.6033662 |
| inclination: | 26.4847° |
| perigee height: | 264 km |
| apogee height: | 20474 km |
| right ascension of ascending node: | 289.5846° |
| argument of perigee: | 303.0284° |
| revolutions per day: | 4.00559271 |
| mean anomaly at epoch: | 20.8793° |
| orbit number at epoch: | 29993 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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