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 67931U 26145.44522106 +.00000000 +00000-0 +24159-3 0 00005
2 67931 43.0017 171.5358 0001341 268.5577 91.5121 15.27585091 04
| Epoch (UTC): | 25 May 2026 10:41:07 |
| Eccentricity: | 0.0001341 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.5358° |
| argument of perigee: | 268.5577° |
| revolutions per day: | 15.27585091 |
| mean anomaly at epoch: | 91.5121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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