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 56509U 26145.46083322 +.00000000 +00000-0 -89860-4 0 00000
2 56509 43.0027 138.6798 0001388 264.9114 95.1580 15.27584018 01
| Epoch (UTC): | 25 May 2026 11:03:35 |
| Eccentricity: | 0.0001388 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 138.6798° |
| argument of perigee: | 264.9114° |
| revolutions per day: | 15.27584018 |
| mean anomaly at epoch: | 95.1580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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