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 32791U 08021J 24357.86529601 .00019591 00000-0 11544-2 0 9993
2 32791 97.7126 329.1943 0006639 44.2956 315.8804 15.11614335904946
| Epoch (UTC): | 22 December 2024 20:46:01 |
| Eccentricity: | 0.0006639 |
| inclination: | 97.7126° |
| perigee height: | 526 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 329.1943° |
| argument of perigee: | 44.2956° |
| revolutions per day: | 15.11614335 |
| mean anomaly at epoch: | 315.8804° |
| orbit number at epoch: | 90494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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