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 43711U 26145.00352139 +.00000000 +00000-0 +14954-3 0 00006
2 43711 97.3601 159.3679 0011523 224.9478 135.0830 15.29430443 07
| Epoch (UTC): | 25 May 2026 00:05:04 |
| Eccentricity: | 0.0011523 |
| inclination: | 97.3601° |
| perigee height: | 470 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 159.3679° |
| argument of perigee: | 224.9478° |
| revolutions per day: | 15.29430443 |
| mean anomaly at epoch: | 135.0830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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