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 56385U 26145.28832941 +.00000000 +00000-0 +42657-4 0 00003
2 56385 43.0035 125.3739 0001290 267.0692 93.0012 15.27580373 04
| Epoch (UTC): | 25 May 2026 06:55:11 |
| Eccentricity: | 0.0001290 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 125.3739° |
| argument of perigee: | 267.0692° |
| revolutions per day: | 15.27580373 |
| mean anomaly at epoch: | 93.0012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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