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 26074.00894258 +.00000000 +00000-0 +41589-3 0 00009
2 40908 97.4803 107.4190 0006086 221.8055 138.2730 15.48245624 04
| Epoch (UTC): | 15 March 2026 00:12:52 |
| Eccentricity: | 0.0006086 |
| inclination: | 97.4803° |
| perigee height: | 418 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 107.4190° |
| argument of perigee: | 221.8055° |
| revolutions per day: | 15.48245624 |
| mean anomaly at epoch: | 138.2730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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