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 67466U 26144.96567580 +.00000000 +00000-0 +55852-3 0 00003
2 67466 43.0030 134.8062 0001362 289.0278 71.0426 15.27594625 09
| Epoch (UTC): | 24 May 2026 23:10:34 |
| Eccentricity: | 0.0001362 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 134.8062° |
| argument of perigee: | 289.0278° |
| revolutions per day: | 15.27594625 |
| mean anomaly at epoch: | 71.0426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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