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 57411U 26145.53320420 +.00000000 +00000-0 +98204-5 0 00006
2 57411 43.0053 174.4849 0001777 275.2122 84.8527 15.27579139 08
| Epoch (UTC): | 25 May 2026 12:47:48 |
| Eccentricity: | 0.0001777 |
| inclination: | 43.0053° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 174.4849° |
| argument of perigee: | 275.2122° |
| revolutions per day: | 15.27579139 |
| mean anomaly at epoch: | 84.8527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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