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 19531U 88089A 23151.51087390 .00000053 00000-0 48187-4 0 9997
2 19531 98.4649 127.2000 0009950 254.7391 105.2684 14.15399879790050
| Epoch (UTC): | 31 May 2023 12:15:39 |
| Eccentricity: | 0.0009950 |
| inclination: | 98.4649° |
| perigee height: | 834 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 127.2000° |
| argument of perigee: | 254.7391° |
| revolutions per day: | 14.15399879 |
| mean anomaly at epoch: | 105.2684° |
| orbit number at epoch: | 79005 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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