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 33591U 09005A 25166.15032149 .00000158 00000-0 10834-3 0 9993
2 33591 98.9970 230.8860 0013451 352.7532 7.3443 14.13376929842890
| Epoch (UTC): | 15 June 2025 03:36:27 |
| Eccentricity: | 0.0013451 |
| inclination: | 98.9970° |
| perigee height: | 838 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 230.8860° |
| argument of perigee: | 352.7532° |
| revolutions per day: | 14.13376929 |
| mean anomaly at epoch: | 7.3443° |
| orbit number at epoch: | 84289 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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