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 26111.65303830 +.00000000 +00000-0 +21172-3 0 00009
2 43806 97.4041 160.5050 0008178 153.8764 206.2883 15.15246893 06
| Epoch (UTC): | 21 April 2026 15:40:22 |
| Eccentricity: | 0.0008178 |
| inclination: | 97.4041° |
| perigee height: | 515 km |
| apogee height: | 526 km |
| right ascension of ascending node: | 160.5050° |
| argument of perigee: | 153.8764° |
| revolutions per day: | 15.15246893 |
| mean anomaly at epoch: | 206.2883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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