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 23334.46929691 .00007788 00000-0 73379-3 0 9999
2 32785 97.7304 297.2452 0009664 272.8578 87.1536 14.94055333845703
| Epoch (UTC): | 30 November 2023 11:15:47 |
| Eccentricity: | 0.0009664 |
| inclination: | 97.7304° |
| perigee height: | 578 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 297.2452° |
| argument of perigee: | 272.8578° |
| revolutions per day: | 14.94055333 |
| mean anomaly at epoch: | 87.1536° |
| orbit number at epoch: | 84570 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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