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 43909U 26145.51568991 +.00000000 +00000-0 +10477-3 0 00002
2 43909 50.0078 140.4456 0000257 247.3549 112.7339 14.29010116 00
| Epoch (UTC): | 25 May 2026 12:22:35 |
| Eccentricity: | 0.0000257 |
| inclination: | 50.0078° |
| perigee height: | 795 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 140.4456° |
| argument of perigee: | 247.3549° |
| revolutions per day: | 14.29010116 |
| mean anomaly at epoch: | 112.7339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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