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 66324U 26145.35697206 +.00000000 +00000-0 +34055-3 0 00000
2 66324 43.0021 139.1962 0001440 270.3269 89.7418 15.27592961 06
| Epoch (UTC): | 25 May 2026 08:34:02 |
| Eccentricity: | 0.0001440 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.1962° |
| argument of perigee: | 270.3269° |
| revolutions per day: | 15.27592961 |
| mean anomaly at epoch: | 89.7418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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