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 67585U 26145.63299722 +.00000000 +00000-0 +57790-3 0 00003
2 67585 97.2845 205.9241 0000250 209.4300 150.6929 15.33462844 08
| Epoch (UTC): | 25 May 2026 15:11:30 |
| Eccentricity: | 0.0000250 |
| inclination: | 97.2845° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.9241° |
| argument of perigee: | 209.4300° |
| revolutions per day: | 15.33462844 |
| mean anomaly at epoch: | 150.6929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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