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 23331.85729814 .00007617 00000-0 71862-3 0 9990
2 32785 97.7292 294.6751 0009637 283.2003 76.8141 14.94011331845247
| Epoch (UTC): | 27 November 2023 20:34:30 |
| Eccentricity: | 0.0009637 |
| inclination: | 97.7292° |
| perigee height: | 579 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 294.6751° |
| argument of perigee: | 283.2003° |
| revolutions per day: | 14.94011331 |
| mean anomaly at epoch: | 76.8141° |
| orbit number at epoch: | 84524 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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