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 32959U 08026B 24278.69584456 .00001099 00000-0 33698-3 0 9995
2 32959 98.9418 312.3554 0068611 316.7857 151.4890 14.42554764860601
| Epoch (UTC): | 04 October 2024 16:42:00 |
| Eccentricity: | 0.0068611 |
| inclination: | 98.9418° |
| perigee height: | 701 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 312.3554° |
| argument of perigee: | 316.7857° |
| revolutions per day: | 14.42554764 |
| mean anomaly at epoch: | 151.4890° |
| orbit number at epoch: | 86060 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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