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 31132U 26103.92908196 +.00000000 +00000-0 +11597-3 0 00005
2 31132 98.4340 86.9962 0071727 164.0602 196.2882 14.66488674 03
| Epoch (UTC): | 13 April 2026 22:17:52 |
| Eccentricity: | 0.0071727 |
| inclination: | 98.4340° |
| perigee height: | 622 km |
| apogee height: | 723 km |
| right ascension of ascending node: | 86.9962° |
| argument of perigee: | 164.0602° |
| revolutions per day: | 14.66488674 |
| mean anomaly at epoch: | 196.2882° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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