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 59328U 26145.29483799 +.00000000 +00000-0 +31223-4 0 00004
2 59328 43.0031 114.5568 0001146 269.9849 90.0871 15.27578369 07
| Epoch (UTC): | 25 May 2026 07:04:34 |
| Eccentricity: | 0.0001146 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.5568° |
| argument of perigee: | 269.9849° |
| revolutions per day: | 15.27578369 |
| mean anomaly at epoch: | 90.0871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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