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 23089.12523758 .00008382 00000-0 83972-3 0 9994
2 32785 97.6981 56.8499 0012801 15.9449 344.2171 14.91557957809105
| Epoch (UTC): | 30 March 2023 03:00:20 |
| Eccentricity: | 0.0012801 |
| inclination: | 97.6981° |
| perigee height: | 584 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 56.8499° |
| argument of perigee: | 15.9449° |
| revolutions per day: | 14.91557957 |
| mean anomaly at epoch: | 344.2171° |
| orbit number at epoch: | 80910 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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