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 17293.52590563 .00000034 00000-0 35639-4 0 9997
2 32958 98.3999 315.8902 0008395 279.2998 80.7235 14.19677957487117
| Epoch (UTC): | 20 October 2017 12:37:18 |
| Eccentricity: | 0.0008395 |
| inclination: | 98.3999° |
| perigee height: | 820 km |
| apogee height: | 832 km |
| right ascension of ascending node: | 315.8902° |
| argument of perigee: | 279.2998° |
| revolutions per day: | 14.19677957 |
| mean anomaly at epoch: | 80.7235° |
| orbit number at epoch: | 48711 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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