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 40967U 26138.10005874 +.00000000 +00000-0 +21248-3 0 00004
2 40967 64.7765 12.4727 0129183 68.3958 293.0860 14.90778967 05
| Epoch (UTC): | 18 May 2026 02:24:05 |
| Eccentricity: | 0.0129183 |
| inclination: | 64.7765° |
| perigee height: | 505 km |
| apogee height: | 686 km |
| right ascension of ascending node: | 12.4727° |
| argument of perigee: | 68.3958° |
| revolutions per day: | 14.90778967 |
| mean anomaly at epoch: | 293.0860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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