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 32956U 08025D 25012.91208511 .00000004 00000-0 -41941-4 0 9995
2 32956 82.5090 321.1865 0021407 13.3642 346.8000 12.43054188755071
| Epoch (UTC): | 12 January 2025 21:53:24 |
| Eccentricity: | 0.0021407 |
| inclination: | 82.5090° |
| perigee height: | 1477 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 321.1865° |
| argument of perigee: | 13.3642° |
| revolutions per day: | 12.43054188 |
| mean anomaly at epoch: | 346.8000° |
| orbit number at epoch: | 75507 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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