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 57123U 26145.66668980 +.00000000 +00000-0 +19910-2 0 00000
2 57123 43.0009 206.8336 0001809 281.5123 122.6149 15.27567422 00
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001809 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 206.8336° |
| argument of perigee: | 281.5123° |
| revolutions per day: | 15.27567422 |
| mean anomaly at epoch: | 122.6149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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