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 32958U 08026A 14204.07765793 .00000005 00000-0 22335-4 0 1949
2 32958 098.5521 261.7025 0010396 109.9972 250.2330 14.19459703318930
| Epoch (UTC): | 23 July 2014 01:51:49 |
| Eccentricity: | 0.0010396 |
| inclination: | 98.5521° |
| perigee height: | 819 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 261.7025° |
| argument of perigee: | 109.9972° |
| revolutions per day: | 14.19459703 |
| mean anomaly at epoch: | 250.2330° |
| orbit number at epoch: | 31893 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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