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 66956U 26145.37919872 +.00000000 +00000-0 +52709-4 0 00006
2 66956 86.4932 290.0863 0003041 93.9684 266.1797 13.24412867 07
| Epoch (UTC): | 25 May 2026 09:06:02 |
| Eccentricity: | 0.0003041 |
| inclination: | 86.4932° |
| perigee height: | 1166 km |
| apogee height: | 1170 km |
| right ascension of ascending node: | 290.0863° |
| argument of perigee: | 93.9684° |
| revolutions per day: | 13.24412867 |
| mean anomaly at epoch: | 266.1797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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