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 57781U 26145.42340128 +.00000000 +00000-0 -70991-4 0 00004
2 57781 43.0001 121.0033 0001063 256.8464 103.2269 15.27579913 05
| Epoch (UTC): | 25 May 2026 10:09:41 |
| Eccentricity: | 0.0001063 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.0033° |
| argument of perigee: | 256.8464° |
| revolutions per day: | 15.27579913 |
| mean anomaly at epoch: | 103.2269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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