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 43226U 26129.15739183 +.00000000 +00000-0 +00000-0 0 00007
2 43226 0.8376 86.2469 0000674 320.5359 147.3699 1.00271184 05
| Epoch (UTC): | 09 May 2026 03:46:38 |
| Eccentricity: | 0.0000674 |
| inclination: | 0.8376° |
| perigee height: | 35784 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 86.2469° |
| argument of perigee: | 320.5359° |
| revolutions per day: | 1.00271184 |
| mean anomaly at epoch: | 147.3699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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