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 11326U 79030A 25318.63773014 .00000113 00000-0 10113-3 0 9996
2 11326 82.9505 204.7080 0028940 342.3095 83.1339 13.75632938572899
| Epoch (UTC): | 14 November 2025 15:18:19 |
| Eccentricity: | 0.0028940 |
| inclination: | 82.9505° |
| perigee height: | 958 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 204.7080° |
| argument of perigee: | 342.3095° |
| revolutions per day: | 13.75632938 |
| mean anomaly at epoch: | 83.1339° |
| orbit number at epoch: | 57289 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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