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 35931U 26145.61001603 +.00000000 +00000-0 +28397-3 0 00001
2 35931 98.2309 134.7156 0014606 305.1099 54.8698 13.99655371 04
| Epoch (UTC): | 25 May 2026 14:38:25 |
| Eccentricity: | 0.0014606 |
| inclination: | 98.2309° |
| perigee height: | 884 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 134.7156° |
| argument of perigee: | 305.1099° |
| revolutions per day: | 13.99655371 |
| mean anomaly at epoch: | 54.8698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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