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 67285U 26145.44363362 +.00000000 +00000-0 +27883-3 0 00001
2 67285 97.3924 220.5944 0011912 83.7651 276.4943 15.23376257 00
| Epoch (UTC): | 25 May 2026 10:38:49 |
| Eccentricity: | 0.0011912 |
| inclination: | 97.3924° |
| perigee height: | 487 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 220.5944° |
| argument of perigee: | 83.7651° |
| revolutions per day: | 15.23376257 |
| mean anomaly at epoch: | 276.4943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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