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 23151.29149011 .00050438 00000-0 14846-2 0 9994
2 32789 97.3037 172.9140 0008594 162.0794 198.0754 15.34864393824890
| Epoch (UTC): | 31 May 2023 06:59:44 |
| Eccentricity: | 0.0008594 |
| inclination: | 97.3037° |
| perigee height: | 455 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 172.9140° |
| argument of perigee: | 162.0794° |
| revolutions per day: | 15.34864393 |
| mean anomaly at epoch: | 198.0754° |
| orbit number at epoch: | 82489 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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