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 57310U 26145.40676029 +.00000000 +00000-0 +52342-4 0 00001
2 57310 43.0023 121.2073 0001173 266.6411 93.4306 15.27577640 03
| Epoch (UTC): | 25 May 2026 09:45:44 |
| Eccentricity: | 0.0001173 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.2073° |
| argument of perigee: | 266.6411° |
| revolutions per day: | 15.27577640 |
| mean anomaly at epoch: | 93.4306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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