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 26109.21829729 +.00000000 +00000-0 +28849-3 0 00006
2 40908 97.4732 143.8793 0008913 105.5152 254.7084 15.49488528 04
| Epoch (UTC): | 19 April 2026 05:14:20 |
| Eccentricity: | 0.0008913 |
| inclination: | 97.4732° |
| perigee height: | 412 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 143.8793° |
| argument of perigee: | 105.5152° |
| revolutions per day: | 15.49488528 |
| mean anomaly at epoch: | 254.7084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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