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 23160.68701797 .00003062 00000-0 30522-3 0 9999
2 32785 97.7055 126.8031 0013561 123.9525 236.2985 14.92233629819705
| Epoch (UTC): | 09 June 2023 16:29:18 |
| Eccentricity: | 0.0013561 |
| inclination: | 97.7055° |
| perigee height: | 581 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 126.8031° |
| argument of perigee: | 123.9525° |
| revolutions per day: | 14.92233629 |
| mean anomaly at epoch: | 236.2985° |
| orbit number at epoch: | 81970 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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