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 26032.39373249 +.00000000 +00000-0 +19869-3 0 00005
2 39425 97.8067 341.9183 0046682 14.7243 345.5321 14.87292072 03
| Epoch (UTC): | 01 February 2026 09:26:58 |
| Eccentricity: | 0.0046682 |
| inclination: | 97.8067° |
| perigee height: | 574 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 341.9183° |
| argument of perigee: | 14.7243° |
| revolutions per day: | 14.87292072 |
| mean anomaly at epoch: | 345.5321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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