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 24357.89361790 .00009506 00000-0 74657-3 0 9992
2 32785 97.7707 322.4359 0012753 78.0888 282.1765 15.01056723903743
| Epoch (UTC): | 22 December 2024 21:26:48 |
| Eccentricity: | 0.0012753 |
| inclination: | 97.7707° |
| perigee height: | 555 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 322.4359° |
| argument of perigee: | 78.0888° |
| revolutions per day: | 15.01056723 |
| mean anomaly at epoch: | 282.1765° |
| orbit number at epoch: | 90374 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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