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 24126U 94029FZ 24357.47396640 .00006401 00000-0 14065-2 0 9998
2 24126 81.8031 141.3195 0297839 5.2380 53.2685 14.33381725476089
| Epoch (UTC): | 22 December 2024 11:22:30 |
| Eccentricity: | 0.0297839 |
| inclination: | 81.8031° |
| perigee height: | 567 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 141.3195° |
| argument of perigee: | 5.2380° |
| revolutions per day: | 14.33381725 |
| mean anomaly at epoch: | 53.2685° |
| orbit number at epoch: | 47608 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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