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 23333.46469093 .00007527 00000-0 70974-3 0 9992
2 32785 97.7303 296.2563 0009632 277.0098 83.0027 14.94038386845555
| Epoch (UTC): | 29 November 2023 11:09:09 |
| Eccentricity: | 0.0009632 |
| inclination: | 97.7303° |
| perigee height: | 578 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 296.2563° |
| argument of perigee: | 277.0098° |
| revolutions per day: | 14.94038386 |
| mean anomaly at epoch: | 83.0027° |
| orbit number at epoch: | 84555 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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