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 26069.93693139 +.00000000 +00000-0 +40012-3 0 00000
2 40908 97.4809 103.2049 0005752 239.4779 120.5904 15.48079231 00
| Epoch (UTC): | 10 March 2026 22:29:10 |
| Eccentricity: | 0.0005752 |
| inclination: | 97.4809° |
| perigee height: | 418 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 103.2049° |
| argument of perigee: | 239.4779° |
| revolutions per day: | 15.48079231 |
| mean anomaly at epoch: | 120.5904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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