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 57344U 26145.54557413 +.00000000 +00000-0 +56444-4 0 00005
2 57344 43.0028 178.0881 0001672 290.9960 69.0713 15.27580163 00
| Epoch (UTC): | 25 May 2026 13:05:37 |
| Eccentricity: | 0.0001672 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 178.0881° |
| argument of perigee: | 290.9960° |
| revolutions per day: | 15.27580163 |
| mean anomaly at epoch: | 69.0713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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