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 17229.88361958 .00000003 00000-0 20823-4 0 9994
2 32958 98.4043 255.4708 0010905 99.1881 261.0529 14.19669433478087
| Epoch (UTC): | 17 August 2017 21:12:24 |
| Eccentricity: | 0.0010905 |
| inclination: | 98.4043° |
| perigee height: | 818 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 255.4708° |
| argument of perigee: | 99.1881° |
| revolutions per day: | 14.19669433 |
| mean anomaly at epoch: | 261.0529° |
| orbit number at epoch: | 47808 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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