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 08294U 75087B 25189.56693248 -.00000141 00000-0 -84271-4 0 9992
2 08294 81.2097 33.2016 0102629 19.0293 341.4667 14.09033866559001
| Epoch (UTC): | 08 July 2025 13:36:22 |
| Eccentricity: | 0.0102629 |
| inclination: | 81.2097° |
| perigee height: | 788 km |
| apogee height: | 937 km |
| right ascension of ascending node: | 33.2016° |
| argument of perigee: | 19.0293° |
| revolutions per day: | 14.09033866 |
| mean anomaly at epoch: | 341.4667° |
| orbit number at epoch: | 55900 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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