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 32789U 08021G 23150.05274224 .00044577 00000-0 13184-2 0 9993
2 32789 97.3040 171.6873 0008453 165.2221 194.9271 15.34744919824606
| Epoch (UTC): | 30 May 2023 01:15:56 |
| Eccentricity: | 0.0008453 |
| inclination: | 97.3040° |
| perigee height: | 456 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 171.6873° |
| argument of perigee: | 165.2221° |
| revolutions per day: | 15.34744919 |
| mean anomaly at epoch: | 194.9271° |
| orbit number at epoch: | 82460 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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