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 32785U 08021C 23148.14732805 .00002259 00000-0 22723-3 0 9991
2 32785 97.7046 114.5355 0012580 162.1477 198.0186 14.92149380817907
| Epoch (UTC): | 28 May 2023 03:32:09 |
| Eccentricity: | 0.0012580 |
| inclination: | 97.7046° |
| perigee height: | 582 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 114.5355° |
| argument of perigee: | 162.1477° |
| revolutions per day: | 14.92149380 |
| mean anomaly at epoch: | 198.0186° |
| orbit number at epoch: | 81790 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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