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 57338U 26145.66668980 +.00000000 +00000-0 +41678-3 0 00005
2 57338 43.0013 177.8732 0000737 271.1280 197.6260 15.27583717 09
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0000737 |
| inclination: | 43.0013° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 177.8732° |
| argument of perigee: | 271.1280° |
| revolutions per day: | 15.27583717 |
| mean anomaly at epoch: | 197.6260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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