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 40908U 26110.96191940 +.00000000 +00000-0 +28726-3 0 00001
2 40908 97.4732 145.6862 0008920 100.7752 259.4504 15.49541273 08
| Epoch (UTC): | 20 April 2026 23:05:09 |
| Eccentricity: | 0.0008920 |
| inclination: | 97.4732° |
| perigee height: | 412 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 145.6862° |
| argument of perigee: | 100.7752° |
| revolutions per day: | 15.49541273 |
| mean anomaly at epoch: | 259.4504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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