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 67944U 26145.26485622 +.00000000 +00000-0 +57173-3 0 00002
2 67944 43.0015 118.1078 0001726 271.0798 88.9856 15.27593187 03
| Epoch (UTC): | 25 May 2026 06:21:23 |
| Eccentricity: | 0.0001726 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 118.1078° |
| argument of perigee: | 271.0798° |
| revolutions per day: | 15.27593187 |
| mean anomaly at epoch: | 88.9856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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