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 67341U 26145.38213286 +.00000000 +00000-0 +40075-3 0 00004
2 67341 43.0007 153.8948 0001417 272.3019 87.7670 15.27589547 00
| Epoch (UTC): | 25 May 2026 09:10:16 |
| Eccentricity: | 0.0001417 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.8948° |
| argument of perigee: | 272.3019° |
| revolutions per day: | 15.27589547 |
| mean anomaly at epoch: | 87.7670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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