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 67817U 26145.49373965 +.00000000 +00000-0 +28998-3 0 00005
2 67817 97.2862 333.6224 0001732 88.3387 271.8054 15.33401704 03
| Epoch (UTC): | 25 May 2026 11:50:59 |
| Eccentricity: | 0.0001732 |
| inclination: | 97.2862° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.6224° |
| argument of perigee: | 88.3387° |
| revolutions per day: | 15.33401704 |
| mean anomaly at epoch: | 271.8054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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