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 25544U 98067A 23030.73101094 .00014801 00000-0 26399-3 0 9999
2 25544 51.6430 289.3774 0004529 290.9765 165.0930 15.50300713380470
| Epoch (UTC): | 30 January 2023 17:32:39 |
| Eccentricity: | 0.0004529 |
| inclination: | 51.6430° |
| perigee height: | 413 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 289.3774° |
| argument of perigee: | 290.9765° |
| revolutions per day: | 15.50300713 |
| mean anomaly at epoch: | 165.0930° |
| orbit number at epoch: | 38047 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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