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 is defined by the following mean orbital elements,
1 32476U 08002A 25290.40158491 0.00001300 00000-0 37535-3 0 05
2 32476 40.0396 3.5722 0012000 106.5973 253.9794 14.43910288 08
| Epoch (UTC): | 17 October 2025 09:38:16 |
| Eccentricity: | 0.0012000 |
| inclination: | 40.0396° |
| perigee height: | 737 km |
| apogee height: | 754 km |
| right ascension of ascending node: | 3.5722° |
| argument of perigee: | 106.5973° |
| revolutions per day: | 14.43910288 |
| mean anomaly at epoch: | 253.9794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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