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 11267U 79011B 25188.87526336 .00000466 00000-0 43872-4 0 9993
2 11267 82.5254 328.7439 0016844 150.6745 209.5423 14.91508808513482
| Epoch (UTC): | 07 July 2025 21:00:22 |
| Eccentricity: | 0.0016844 |
| inclination: | 82.5254° |
| perigee height: | 581 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 328.7439° |
| argument of perigee: | 150.6745° |
| revolutions per day: | 14.91508808 |
| mean anomaly at epoch: | 209.5423° |
| orbit number at epoch: | 51348 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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