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 39425U 26145.13778271 +.00000000 +00000-0 +10959-3 0 00007
2 39425 97.8210 92.9300 0046110 3.7587 356.3966 14.87594708 08
| Epoch (UTC): | 25 May 2026 03:18:24 |
| Eccentricity: | 0.0046110 |
| inclination: | 97.8210° |
| perigee height: | 573 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 92.9300° |
| argument of perigee: | 3.7587° |
| revolutions per day: | 14.87594708 |
| mean anomaly at epoch: | 356.3966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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