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 67866U 26145.55608427 +.00000000 +00000-0 +61583-3 0 00007
2 67866 53.1585 207.2493 0001189 60.5468 299.5651 15.30208420 09
| Epoch (UTC): | 25 May 2026 13:20:45 |
| Eccentricity: | 0.0001189 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.2493° |
| argument of perigee: | 60.5468° |
| revolutions per day: | 15.30208420 |
| mean anomaly at epoch: | 299.5651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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