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 11574U 79089B 25193.88389502 .00000069 00000-0 28844-4 0 9999
2 11574 74.0677 174.8588 0014799 44.5571 315.6772 14.42151437401534
| Epoch (UTC): | 12 July 2025 21:12:48 |
| Eccentricity: | 0.0014799 |
| inclination: | 74.0677° |
| perigee height: | 741 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 174.8588° |
| argument of perigee: | 44.5571° |
| revolutions per day: | 14.42151437 |
| mean anomaly at epoch: | 315.6772° |
| orbit number at epoch: | 40153 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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