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 26150.61403934 +.00000000 +00000-0 +26034-3 0 00006
2 35931 98.2314 139.2193 0014496 290.0461 69.9145 13.99659456 05
| Epoch (UTC): | 30 May 2026 14:44:12 |
| Eccentricity: | 0.0014496 |
| inclination: | 98.2314° |
| perigee height: | 884 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 139.2193° |
| argument of perigee: | 290.0461° |
| revolutions per day: | 13.99659456 |
| mean anomaly at epoch: | 69.9145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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