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 19071U 88033B 23273.18917432 .00000122 00000-0 23227-3 0 9996
2 19071 90.3247 351.6870 0186506 244.9820 183.2450 13.27770791715886
| Epoch (UTC): | 30 September 2023 04:32:24 |
| Eccentricity: | 0.0186506 |
| inclination: | 90.3247° |
| perigee height: | 1014 km |
| apogee height: | 1295 km |
| right ascension of ascending node: | 351.6870° |
| argument of perigee: | 244.9820° |
| revolutions per day: | 13.27770791 |
| mean anomaly at epoch: | 183.2450° |
| orbit number at epoch: | 71588 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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