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 43111U 26145.61676500 +.00000000 +00000-0 +36066-3 0 00006
2 43111 97.4800 205.4697 0001037 49.5093 310.6232 15.19271404 05
| Epoch (UTC): | 25 May 2026 14:48:08 |
| Eccentricity: | 0.0001037 |
| inclination: | 97.4800° |
| perigee height: | 507 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 205.4697° |
| argument of perigee: | 49.5093° |
| revolutions per day: | 15.19271404 |
| mean anomaly at epoch: | 310.6232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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