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 26145.40683681 +.00000000 +00000-0 +11788-3 0 00008
2 39425 97.8210 93.1952 0046079 2.8818 357.2655 14.87595665 03
| Epoch (UTC): | 25 May 2026 09:45:50 |
| Eccentricity: | 0.0046079 |
| inclination: | 97.8210° |
| perigee height: | 573 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 93.1952° |
| argument of perigee: | 2.8818° |
| revolutions per day: | 14.87595665 |
| mean anomaly at epoch: | 357.2655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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