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 26066.51093247 +.00000000 +00000-0 +47591-3 0 00004
2 40908 97.4809 99.6594 0005619 255.7902 104.2724 15.47926064 07
| Epoch (UTC): | 07 March 2026 12:15:44 |
| Eccentricity: | 0.0005619 |
| inclination: | 97.4809° |
| perigee height: | 419 km |
| apogee height: | 427 km |
| right ascension of ascending node: | 99.6594° |
| argument of perigee: | 255.7902° |
| revolutions per day: | 15.47926064 |
| mean anomaly at epoch: | 104.2724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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