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 56516U 26145.46469218 +.00000000 +00000-0 +56999-5 0 00007
2 56516 43.0031 138.7092 0001390 266.8946 93.1747 15.27579260 05
| Epoch (UTC): | 25 May 2026 11:09:09 |
| Eccentricity: | 0.0001390 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 138.7092° |
| argument of perigee: | 266.8946° |
| revolutions per day: | 15.27579260 |
| mean anomaly at epoch: | 93.1747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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