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 67939U 26145.28284863 +.00000000 +00000-0 +53430-3 0 00004
2 67939 43.0014 118.2642 0001395 278.0252 82.0441 15.27594338 02
| Epoch (UTC): | 25 May 2026 06:47:18 |
| Eccentricity: | 0.0001395 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 118.2642° |
| argument of perigee: | 278.0252° |
| revolutions per day: | 15.27594338 |
| mean anomaly at epoch: | 82.0441° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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