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 67611U 26145.44519941 +.00000000 +00000-0 +76633-3 0 00007
2 67611 97.2857 210.5172 0000695 258.2007 101.9157 15.33471515 02
| Epoch (UTC): | 25 May 2026 10:41:05 |
| Eccentricity: | 0.0000695 |
| inclination: | 97.2857° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.5172° |
| argument of perigee: | 258.2007° |
| revolutions per day: | 15.33471515 |
| mean anomaly at epoch: | 101.9157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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