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 66106U 26145.58335647 +.00000000 +00000-0 -49892-3 0 00007
2 66106 53.1605 106.6122 0001411 94.6161 87.2726 15.34397822 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001411 |
| inclination: | 53.1605° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 106.6122° |
| argument of perigee: | 94.6161° |
| revolutions per day: | 15.34397822 |
| mean anomaly at epoch: | 87.2726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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