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 39232U 13043A 25288.80624759 0.00035000 00000-0 34137-3 0 08
2 39232 97.8940 349.7905 0521296 186.2079 173.7919 14.80106298 09
| Epoch (UTC): | 15 October 2025 19:20:59 |
| Eccentricity: | 0.0521296 |
| inclination: | 97.8940° |
| perigee height: | 264 km |
| apogee height: | 994 km |
| right ascension of ascending node: | 349.7905° |
| argument of perigee: | 186.2079° |
| revolutions per day: | 14.80106298 |
| mean anomaly at epoch: | 173.7919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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