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 67945U 26145.32253571 +.00000000 +00000-0 +39062-3 0 00003
2 67945 43.0026 117.6785 0001848 282.7224 77.3421 15.27589250 09
| Epoch (UTC): | 25 May 2026 07:44:27 |
| Eccentricity: | 0.0001848 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 117.6785° |
| argument of perigee: | 282.7224° |
| revolutions per day: | 15.27589250 |
| mean anomaly at epoch: | 77.3421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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