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 56406U 26145.60773193 +.00000000 +00000-0 +25867-4 0 00000
2 56406 43.0013 113.0302 0000658 248.6428 111.4354 15.27564777 07
| Epoch (UTC): | 25 May 2026 14:35:08 |
| Eccentricity: | 0.0000658 |
| inclination: | 43.0013° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 113.0302° |
| argument of perigee: | 248.6428° |
| revolutions per day: | 15.27564777 |
| mean anomaly at epoch: | 111.4354° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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