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 24259.89209196 .00013451 00000-0 11258-2 0 9995
2 32785 97.7625 224.6000 0011447 31.7208 328.4702 14.98527170889123
| Epoch (UTC): | 15 September 2024 21:24:36 |
| Eccentricity: | 0.0011447 |
| inclination: | 97.7625° |
| perigee height: | 563 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 224.6000° |
| argument of perigee: | 31.7208° |
| revolutions per day: | 14.98527170 |
| mean anomaly at epoch: | 328.4702° |
| orbit number at epoch: | 88912 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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