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 56515U 26145.47497139 +.00000000 +00000-0 +81090-5 0 00000
2 56515 43.0011 138.7864 0001032 273.6140 86.4594 15.27575383 01
| Epoch (UTC): | 25 May 2026 11:23:57 |
| Eccentricity: | 0.0001032 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 138.7864° |
| argument of perigee: | 273.6140° |
| revolutions per day: | 15.27575383 |
| mean anomaly at epoch: | 86.4594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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