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 26072.58701955 +.00000000 +00000-0 +35231-3 0 00008
2 40908 97.4807 105.9474 0005928 227.7194 132.3554 15.48180286 00
| Epoch (UTC): | 13 March 2026 14:05:18 |
| Eccentricity: | 0.0005928 |
| inclination: | 97.4807° |
| perigee height: | 418 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 105.9474° |
| argument of perigee: | 227.7194° |
| revolutions per day: | 15.48180286 |
| mean anomaly at epoch: | 132.3554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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