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 67432U 26145.46675392 +.00000000 +00000-0 +56056-3 0 00000
2 67432 43.0013 164.8013 0001939 278.6522 81.4110 15.27595774 09
| Epoch (UTC): | 25 May 2026 11:12:07 |
| Eccentricity: | 0.0001939 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.8013° |
| argument of perigee: | 278.6522° |
| revolutions per day: | 15.27595774 |
| mean anomaly at epoch: | 81.4110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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