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 19274U 88056A 22146.19183550 .00002357 00000-0 15258-3 0 9998
2 19274 82.5034 195.6572 0008124 281.0862 78.9452 15.07713472846532
| Epoch (UTC): | 26 May 2022 04:36:14 |
| Eccentricity: | 0.0008124 |
| inclination: | 82.5034° |
| perigee height: | 537 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 195.6572° |
| argument of perigee: | 281.0862° |
| revolutions per day: | 15.07713472 |
| mean anomaly at epoch: | 78.9452° |
| orbit number at epoch: | 84653 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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