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 43571U 26145.51876788 +.00000000 +00000-0 +70802-4 0 00002
2 43571 86.3969 66.2340 0002340 84.5914 275.5549 14.34215181 01
| Epoch (UTC): | 25 May 2026 12:27:01 |
| Eccentricity: | 0.0002340 |
| inclination: | 86.3969° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 66.2340° |
| argument of perigee: | 84.5914° |
| revolutions per day: | 14.34215181 |
| mean anomaly at epoch: | 275.5549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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