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 26106.94910100 +.00000000 +00000-0 +13191-2 0 00006
2 40922 82.4835 116.4257 0014641 169.2694 190.8701 12.42882538 07
| Epoch (UTC): | 16 April 2026 22:46:42 |
| Eccentricity: | 0.0014641 |
| inclination: | 82.4835° |
| perigee height: | 1483 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 116.4257° |
| argument of perigee: | 169.2694° |
| revolutions per day: | 12.42882538 |
| mean anomaly at epoch: | 190.8701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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