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 57534U 26145.36774484 +.00000000 +00000-0 +49396-4 0 00003
2 57534 43.0032 135.8580 0001527 277.3857 82.6821 15.27580650 08
| Epoch (UTC): | 25 May 2026 08:49:33 |
| Eccentricity: | 0.0001527 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.8580° |
| argument of perigee: | 277.3857° |
| revolutions per day: | 15.27580650 |
| mean anomaly at epoch: | 82.6821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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