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 27432U 02024C 25189.18508453 .00000025 00000-0 35965-4 0 9994
2 27432 98.9221 238.2809 0050079 358.3270 45.7701 14.14489973194752
| Epoch (UTC): | 08 July 2025 04:26:31 |
| Eccentricity: | 0.0050079 |
| inclination: | 98.9221° |
| perigee height: | 808 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 238.2809° |
| argument of perigee: | 358.3270° |
| revolutions per day: | 14.14489973 |
| mean anomaly at epoch: | 45.7701° |
| orbit number at epoch: | 19475 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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