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 23027.84905010 .00004984 00000-0 31063-3 0 9992
2 19274 82.4914 314.8867 0019619 164.2864 195.8978 15.09181506862501
| Epoch (UTC): | 27 January 2023 20:22:37 |
| Eccentricity: | 0.0019619 |
| inclination: | 82.4914° |
| perigee height: | 525 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 314.8867° |
| argument of perigee: | 164.2864° |
| revolutions per day: | 15.09181506 |
| mean anomaly at epoch: | 195.8978° |
| orbit number at epoch: | 86250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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