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 26083.51692766 +.00000000 +00000-0 +00000-0 0 00001
2 43226 0.7196 87.0333 0001620 229.7413 321.8049 1.00271640 01
| Epoch (UTC): | 24 March 2026 12:24:22 |
| Eccentricity: | 0.0001620 |
| inclination: | 0.7196° |
| perigee height: | 35780 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 87.0333° |
| argument of perigee: | 229.7413° |
| revolutions per day: | 1.00271640 |
| mean anomaly at epoch: | 321.8049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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