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 19211U 88050B 22222.02884688 .00000240 00000-0 26282-4 0 9999
2 19211 82.5238 243.9566 0022864 45.3766 314.9309 14.83267987824336
| Epoch (UTC): | 10 August 2022 00:41:32 |
| Eccentricity: | 0.0022864 |
| inclination: | 82.5238° |
| perigee height: | 603 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 243.9566° |
| argument of perigee: | 45.3766° |
| revolutions per day: | 14.83267987 |
| mean anomaly at epoch: | 314.9309° |
| orbit number at epoch: | 82433 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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