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 56517U 26145.42114630 +.00000000 +00000-0 +11534-4 0 00004
2 56517 43.0011 139.2314 0001039 268.5862 91.4870 15.27576631 00
| Epoch (UTC): | 25 May 2026 10:06:27 |
| Eccentricity: | 0.0001039 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.2314° |
| argument of perigee: | 268.5862° |
| revolutions per day: | 15.27576631 |
| mean anomaly at epoch: | 91.4870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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