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 26150.87021492 +.00000000 +00000-0 +31598-3 0 00009
2 31132 98.4360 135.2559 0071791 19.1953 341.1929 14.66593083 09
| Epoch (UTC): | 30 May 2026 20:53:06 |
| Eccentricity: | 0.0071791 |
| inclination: | 98.4360° |
| perigee height: | 621 km |
| apogee height: | 723 km |
| right ascension of ascending node: | 135.2559° |
| argument of perigee: | 19.1953° |
| revolutions per day: | 14.66593083 |
| mean anomaly at epoch: | 341.1929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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