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 40961U 26145.60655245 +.00000000 +00000-0 +11183-3 0 00001
2 40961 97.6508 146.0958 0016431 342.4533 17.6109 14.78115864 08
| Epoch (UTC): | 25 May 2026 14:33:26 |
| Eccentricity: | 0.0016431 |
| inclination: | 97.6508° |
| perigee height: | 624 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 146.0958° |
| argument of perigee: | 342.4533° |
| revolutions per day: | 14.78115864 |
| mean anomaly at epoch: | 17.6109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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