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 43766U 26145.11585373 +.00000000 +00000-0 +54814-3 0 00005
2 43766 97.4346 208.9129 0007981 25.3456 334.8176 15.34183484 05
| Epoch (UTC): | 25 May 2026 02:46:49 |
| Eccentricity: | 0.0007981 |
| inclination: | 97.4346° |
| perigee height: | 458 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 208.9129° |
| argument of perigee: | 25.3456° |
| revolutions per day: | 15.34183484 |
| mean anomaly at epoch: | 334.8176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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