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 56412U 26145.36529370 +.00000000 +00000-0 +16377-4 0 00002
2 56412 43.0048 113.7964 0001408 287.7775 72.2923 15.27577411 01
| Epoch (UTC): | 25 May 2026 08:46:01 |
| Eccentricity: | 0.0001408 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 113.7964° |
| argument of perigee: | 287.7775° |
| revolutions per day: | 15.27577411 |
| mean anomaly at epoch: | 72.2923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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