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 43256U 26145.36555201 +.00000000 +00000-0 +71601-4 0 00007
2 43256 86.3936 299.8959 0001977 89.3697 270.7726 14.34219281 00
| Epoch (UTC): | 25 May 2026 08:46:23 |
| Eccentricity: | 0.0001977 |
| inclination: | 86.3936° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 299.8959° |
| argument of perigee: | 89.3697° |
| revolutions per day: | 14.34219281 |
| mean anomaly at epoch: | 270.7726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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