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 43186U 18014G 25341.20338851 .00010066 00000-0 55355-3 0 9990
2 43186 97.5491 242.3361 0007901 335.4529 24.6326 15.14248418429688
| Epoch (UTC): | 07 December 2025 04:52:52 |
| Eccentricity: | 0.0007901 |
| inclination: | 97.5491° |
| perigee height: | 518 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 242.3361° |
| argument of perigee: | 335.4529° |
| revolutions per day: | 15.14248418 |
| mean anomaly at epoch: | 24.6326° |
| orbit number at epoch: | 42968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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