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 43184U 18014E 25347.02097363 .00068404 00000-0 11790-2 0 9997
2 43184 97.4886 262.5152 0003541 166.4373 193.6974 15.50814046431900
| Epoch (UTC): | 13 December 2025 00:30:12 |
| Eccentricity: | 0.0003541 |
| inclination: | 97.4886° |
| perigee height: | 412 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 262.5152° |
| argument of perigee: | 166.4373° |
| revolutions per day: | 15.50814046 |
| mean anomaly at epoch: | 193.6974° |
| orbit number at epoch: | 43190 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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