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 15027.56235591 .00000058 00000-0 47397-4 0 7528
2 32958 098.5234 083.4768 0009062 289.8497 070.1707 14.19519818345674
| Epoch (UTC): | 27 January 2015 13:29:47 |
| Eccentricity: | 0.0009062 |
| inclination: | 98.5234° |
| perigee height: | 820 km |
| apogee height: | 833 km |
| right ascension of ascending node: | 83.4768° |
| argument of perigee: | 289.8497° |
| revolutions per day: | 14.19519818 |
| mean anomaly at epoch: | 70.1707° |
| orbit number at epoch: | 34567 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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