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 56505U 26145.43785188 +.00000000 +00000-0 +42835-4 0 00002
2 56505 43.0050 139.3688 0001767 283.9082 76.1573 15.27580162 02
| Epoch (UTC): | 25 May 2026 10:30:30 |
| Eccentricity: | 0.0001767 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.3688° |
| argument of perigee: | 283.9082° |
| revolutions per day: | 15.27580162 |
| mean anomaly at epoch: | 76.1573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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