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 59323U 26145.34270137 +.00000000 +00000-0 +57731-4 0 00007
2 59323 43.0026 121.8370 0001313 272.7542 87.3160 15.27578784 07
| Epoch (UTC): | 25 May 2026 08:13:29 |
| Eccentricity: | 0.0001313 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.8370° |
| argument of perigee: | 272.7542° |
| revolutions per day: | 15.27578784 |
| mean anomaly at epoch: | 87.3160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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