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 26037.60794939 +.00000000 +00000-0 +00000-0 0 00005
2 43226 0.6016 88.1527 0002754 213.0089 324.8756 1.00269924 02
| Epoch (UTC): | 06 February 2026 14:35:26 |
| Eccentricity: | 0.0002754 |
| inclination: | 0.6016° |
| perigee height: | 35776 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 88.1527° |
| argument of perigee: | 213.0089° |
| revolutions per day: | 1.00269924 |
| mean anomaly at epoch: | 324.8756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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