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 56428U 26145.35768012 +.00000000 +00000-0 +34062-4 0 00007
2 56428 43.0053 106.6935 0001685 298.9147 61.1535 15.26743685 00
| Epoch (UTC): | 25 May 2026 08:35:03 |
| Eccentricity: | 0.0001685 |
| inclination: | 43.0053° |
| perigee height: | 484 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 106.6935° |
| argument of perigee: | 298.9147° |
| revolutions per day: | 15.26743685 |
| mean anomaly at epoch: | 61.1535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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