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 26075.23692384 +.00000000 +00000-0 +33286-3 0 00006
2 40908 97.4799 108.6895 0006217 216.6623 143.4202 15.48289307 00
| Epoch (UTC): | 16 March 2026 05:41:10 |
| Eccentricity: | 0.0006217 |
| inclination: | 97.4799° |
| perigee height: | 418 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 108.6895° |
| argument of perigee: | 216.6623° |
| revolutions per day: | 15.48289307 |
| mean anomaly at epoch: | 143.4202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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