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 17191U 86097A 22147.04366602 .00003169 00000-0 17193-3 0 9995
2 17191 82.4766 49.5940 0004325 358.5343 1.5875 15.14220115936477
| Epoch (UTC): | 27 May 2022 01:02:52 |
| Eccentricity: | 0.0004325 |
| inclination: | 82.4766° |
| perigee height: | 520 km |
| apogee height: | 526 km |
| right ascension of ascending node: | 49.5940° |
| argument of perigee: | 358.5343° |
| revolutions per day: | 15.14220115 |
| mean anomaly at epoch: | 1.5875° |
| orbit number at epoch: | 93647 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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