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 67941U 26145.39177183 +.00000000 +00000-0 +70649-3 0 00006
2 67941 43.0005 117.3451 0001155 265.8783 94.1937 15.27601379 08
| Epoch (UTC): | 25 May 2026 09:24:09 |
| Eccentricity: | 0.0001155 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 117.3451° |
| argument of perigee: | 265.8783° |
| revolutions per day: | 15.27601379 |
| mean anomaly at epoch: | 94.1937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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