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 57746U 26145.24070368 +.00000000 +00000-0 -28803-5 0 00007
2 57746 43.0025 96.7444 0000699 276.1110 83.9662 15.27583837 04
| Epoch (UTC): | 25 May 2026 05:46:36 |
| Eccentricity: | 0.0000699 |
| inclination: | 43.0025° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 96.7444° |
| argument of perigee: | 276.1110° |
| revolutions per day: | 15.27583837 |
| mean anomaly at epoch: | 83.9662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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