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 67507U 26145.56608553 +.00000000 +00000-0 +88328-3 0 00006
2 67507 43.0004 239.8437 0001482 275.1456 84.9226 15.27586409 07
| Epoch (UTC): | 25 May 2026 13:35:09 |
| Eccentricity: | 0.0001482 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 239.8437° |
| argument of perigee: | 275.1456° |
| revolutions per day: | 15.27586409 |
| mean anomaly at epoch: | 84.9226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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