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 43678U 18084H 25196.78294656 .00002219 00000-0 19094-3 0 9999
2 43678 98.1066 14.2929 0009007 152.9311 207.2381 14.98464927365804
| Epoch (UTC): | 15 July 2025 18:47:26 |
| Eccentricity: | 0.0009007 |
| inclination: | 98.1066° |
| perigee height: | 565 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 14.2929° |
| argument of perigee: | 152.9311° |
| revolutions per day: | 14.98464927 |
| mean anomaly at epoch: | 207.2381° |
| orbit number at epoch: | 36580 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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