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 56504U 26145.47754426 +.00000000 +00000-0 -12864-4 0 00006
2 56504 43.0003 138.8115 0000934 260.7609 99.3137 15.27577965 01
| Epoch (UTC): | 25 May 2026 11:27:39 |
| Eccentricity: | 0.0000934 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 138.8115° |
| argument of perigee: | 260.7609° |
| revolutions per day: | 15.27577965 |
| mean anomaly at epoch: | 99.3137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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