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 26071.68213050 +.00000000 +00000-0 +36206-3 0 00005
2 40908 97.4808 105.0108 0005876 231.7337 128.3385 15.48147092 07
| Epoch (UTC): | 12 March 2026 16:22:16 |
| Eccentricity: | 0.0005876 |
| inclination: | 97.4808° |
| perigee height: | 418 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 105.0108° |
| argument of perigee: | 231.7337° |
| revolutions per day: | 15.48147092 |
| mean anomaly at epoch: | 128.3385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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