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 57442U 26145.47553098 +.00000000 +00000-0 -49331-4 0 00009
2 57442 43.0008 186.3389 0001434 269.0182 91.0506 15.27574192 01
| Epoch (UTC): | 25 May 2026 11:24:45 |
| Eccentricity: | 0.0001434 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.3389° |
| argument of perigee: | 269.0182° |
| revolutions per day: | 15.27574192 |
| mean anomaly at epoch: | 91.0506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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