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 67446U 26145.43237669 +.00000000 +00000-0 +67389-3 0 00004
2 67446 43.0005 132.2928 0001645 266.0994 93.9670 15.27595058 01
| Epoch (UTC): | 25 May 2026 10:22:37 |
| Eccentricity: | 0.0001645 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.2928° |
| argument of perigee: | 266.0994° |
| revolutions per day: | 15.27595058 |
| mean anomaly at epoch: | 93.9670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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