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 43806U 26075.85609144 +.00000000 +00000-0 +25368-3 0 00008
2 43806 97.4121 125.6145 0005729 293.3383 66.7246 15.14837376 01
| Epoch (UTC): | 16 March 2026 20:32:46 |
| Eccentricity: | 0.0005729 |
| inclination: | 97.4121° |
| perigee height: | 518 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 125.6145° |
| argument of perigee: | 293.3383° |
| revolutions per day: | 15.14837376 |
| mean anomaly at epoch: | 66.7246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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