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 56511U 26145.46726205 +.00000000 +00000-0 +44456-4 0 00008
2 56511 43.0022 138.7237 0001111 269.2693 90.8032 15.27577517 02
| Epoch (UTC): | 25 May 2026 11:12:51 |
| Eccentricity: | 0.0001111 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 138.7237° |
| argument of perigee: | 269.2693° |
| revolutions per day: | 15.27577517 |
| mean anomaly at epoch: | 90.8032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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