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 15063.08730148 .00000100 00000-0 67126-4 0 9996
2 32958 098.5190 117.6695 0009446 178.4147 181.7053 14.19531275350710
| Epoch (UTC): | 04 March 2015 02:05:42 |
| Eccentricity: | 0.0009446 |
| inclination: | 98.5190° |
| perigee height: | 820 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 117.6695° |
| argument of perigee: | 178.4147° |
| revolutions per day: | 14.19531275 |
| mean anomaly at epoch: | 181.7053° |
| orbit number at epoch: | 35071 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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