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 57787U 26145.31447947 +.00000000 +00000-0 +25848-4 0 00005
2 57787 43.0028 121.9081 0001177 278.4017 81.6701 15.27579865 08
| Epoch (UTC): | 25 May 2026 07:32:51 |
| Eccentricity: | 0.0001177 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.9081° |
| argument of perigee: | 278.4017° |
| revolutions per day: | 15.27579865 |
| mean anomaly at epoch: | 81.6701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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