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 40966U 26144.83122257 +.00000000 +00000-0 +31883-3 0 00001
2 40966 64.7631 317.9620 0119825 71.0717 290.3341 14.95524882 01
| Epoch (UTC): | 24 May 2026 19:56:57 |
| Eccentricity: | 0.0119825 |
| inclination: | 64.7631° |
| perigee height: | 497 km |
| apogee height: | 664 km |
| right ascension of ascending node: | 317.9620° |
| argument of perigee: | 71.0717° |
| revolutions per day: | 14.95524882 |
| mean anomaly at epoch: | 290.3341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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