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 26099.14308538 +.00000000 +00000-0 +26133-3 0 00000
2 40908 97.4754 133.4419 0008685 134.3309 225.8655 15.49234715 08
| Epoch (UTC): | 09 April 2026 03:26:02 |
| Eccentricity: | 0.0008685 |
| inclination: | 97.4754° |
| perigee height: | 413 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 133.4419° |
| argument of perigee: | 134.3309° |
| revolutions per day: | 15.49234715 |
| mean anomaly at epoch: | 225.8655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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