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 25981U 26097.14204784 +.00000000 +00000-0 +31433-3 0 00009
2 25981 45.0214 130.9602 0001758 48.4012 311.6987 14.37963567 00
| Epoch (UTC): | 07 April 2026 03:24:32 |
| Eccentricity: | 0.0001758 |
| inclination: | 45.0214° |
| perigee height: | 764 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 130.9602° |
| argument of perigee: | 48.4012° |
| revolutions per day: | 14.37963567 |
| mean anomaly at epoch: | 311.6987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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