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 43946U 26145.62909117 +.00000000 +00000-0 +22802-3 0 00009
2 43946 97.4766 244.4404 0008024 10.1208 350.0190 15.25435560 09
| Epoch (UTC): | 25 May 2026 15:05:53 |
| Eccentricity: | 0.0008024 |
| inclination: | 97.4766° |
| perigee height: | 484 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 244.4404° |
| argument of perigee: | 10.1208° |
| revolutions per day: | 15.25435560 |
| mean anomaly at epoch: | 350.0190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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