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 26097.10987919 +.00000000 +00000-0 +15035-3 0 00001
2 39425 97.8163 45.6054 0046532 158.0833 202.2388 14.87503746 01
| Epoch (UTC): | 07 April 2026 02:38:13 |
| Eccentricity: | 0.0046532 |
| inclination: | 97.8163° |
| perigee height: | 573 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 45.6054° |
| argument of perigee: | 158.0833° |
| revolutions per day: | 14.87503746 |
| mean anomaly at epoch: | 202.2388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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