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 22267.50258500 .00001942 00000-0 20732-3 0 9993
2 32785 97.6687 235.2850 0010879 265.4966 94.5009 14.89895886781300
| Epoch (UTC): | 24 September 2022 12:03:43 |
| Eccentricity: | 0.0010879 |
| inclination: | 97.6687° |
| perigee height: | 590 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 235.2850° |
| argument of perigee: | 265.4966° |
| revolutions per day: | 14.89895886 |
| mean anomaly at epoch: | 94.5009° |
| orbit number at epoch: | 78130 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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