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 32376U 07059A 24281.50720228 .00002879 00000-0 36821-3 0 9994
2 32376 97.8892 103.0252 0001543 91.8263 268.3126 14.82140072910581
| Epoch (UTC): | 07 October 2024 12:10:22 |
| Eccentricity: | 0.0001543 |
| inclination: | 97.8892° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 103.0252° |
| argument of perigee: | 91.8263° |
| revolutions per day: | 14.82140072 |
| mean anomaly at epoch: | 268.3126° |
| orbit number at epoch: | 91058 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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