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 32785U 08021C 25143.90979422 .00004315 00000-0 31444-3 0 9995
2 32785 97.7845 114.9530 0007496 268.8881 91.1485 15.04270228926643
| Epoch (UTC): | 23 May 2025 21:50:06 |
| Eccentricity: | 0.0007496 |
| inclination: | 97.7845° |
| perigee height: | 548 km |
| apogee height: | 559 km |
| right ascension of ascending node: | 114.9530° |
| argument of perigee: | 268.8881° |
| revolutions per day: | 15.04270228 |
| mean anomaly at epoch: | 91.1485° |
| orbit number at epoch: | 92664 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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