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 59336U 26145.19989840 +.00000000 +00000-0 +38665-4 0 00007
2 59336 43.0004 114.6951 0001055 267.2495 92.8236 15.27578777 08
| Epoch (UTC): | 25 May 2026 04:47:51 |
| Eccentricity: | 0.0001055 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.6951° |
| argument of perigee: | 267.2495° |
| revolutions per day: | 15.27578777 |
| mean anomaly at epoch: | 92.8236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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