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 56524U 26145.37375830 +.00000000 +00000-0 -15868-4 0 00002
2 56524 43.0039 139.7414 0001755 287.3498 72.7162 15.27570122 08
| Epoch (UTC): | 25 May 2026 08:58:12 |
| Eccentricity: | 0.0001755 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.7414° |
| argument of perigee: | 287.3498° |
| revolutions per day: | 15.27570122 |
| mean anomaly at epoch: | 72.7162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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