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 19460U 88078A 22088.78120934 0.00000082 00000-0 29674-4 0 00
2 19460 84.9771 288.0494 0003496 22.5263 337.4736 14.33562404 00
| Epoch (UTC): | 29 March 2022 18:44:56 |
| Eccentricity: | 0.0003496 |
| inclination: | 84.9771° |
| perigee height: | 777 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 288.0494° |
| argument of perigee: | 22.5263° |
| revolutions per day: | 14.33562404 |
| mean anomaly at epoch: | 337.4736° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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