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 40922U 26053.82140627 +.00000000 +00000-0 +77396-3 0 00001
2 40922 82.4918 149.5145 0013254 291.2329 68.7335 12.42930149 00
| Epoch (UTC): | 22 February 2026 19:42:49 |
| Eccentricity: | 0.0013254 |
| inclination: | 82.4918° |
| perigee height: | 1484 km |
| apogee height: | 1505 km |
| right ascension of ascending node: | 149.5145° |
| argument of perigee: | 291.2329° |
| revolutions per day: | 12.42930149 |
| mean anomaly at epoch: | 68.7335° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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