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 23332.46007366 .00007683 00000-0 72459-3 0 9995
2 32785 97.7298 295.2679 0009630 280.8334 79.1802 14.94021795845405
| Epoch (UTC): | 28 November 2023 11:02:30 |
| Eccentricity: | 0.0009630 |
| inclination: | 97.7298° |
| perigee height: | 579 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 295.2679° |
| argument of perigee: | 280.8334° |
| revolutions per day: | 14.94021795 |
| mean anomaly at epoch: | 79.1802° |
| orbit number at epoch: | 84540 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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