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 20547U 90028B 17229.26755720 .00000552 00000-0 21395-4 0 9998
2 20547 94.1068 162.5315 0085796 33.9053 326.7634 15.23926981508481
| Epoch (UTC): | 17 August 2017 06:25:16 |
| Eccentricity: | 0.0085796 |
| inclination: | 94.1068° |
| perigee height: | 435 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 162.5315° |
| argument of perigee: | 33.9053° |
| revolutions per day: | 15.23926981 |
| mean anomaly at epoch: | 326.7634° |
| orbit number at epoch: | 50848 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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