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 25131.93797842 .00002287 00000-0 19796-3 0 9994
2 43678 98.1008 306.9753 0008468 25.7924 334.3718 14.98198735356091
| Epoch (UTC): | 11 May 2025 22:30:41 |
| Eccentricity: | 0.0008468 |
| inclination: | 98.1008° |
| perigee height: | 566 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 306.9753° |
| argument of perigee: | 25.7924° |
| revolutions per day: | 14.98198735 |
| mean anomaly at epoch: | 334.3718° |
| orbit number at epoch: | 35609 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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