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 67904U 26145.42867235 +.00000000 +00000-0 +44257-3 0 00009
2 67904 43.0004 172.3133 0001526 270.5241 89.5436 15.27588879 09
| Epoch (UTC): | 25 May 2026 10:17:17 |
| Eccentricity: | 0.0001526 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 172.3133° |
| argument of perigee: | 270.5241° |
| revolutions per day: | 15.27588879 |
| mean anomaly at epoch: | 89.5436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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