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 57418U 26145.57719090 +.00000000 +00000-0 +63184-4 0 00000
2 57418 43.0016 181.6319 0002000 270.1585 89.9037 15.27578997 06
| Epoch (UTC): | 25 May 2026 13:51:09 |
| Eccentricity: | 0.0002000 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 181.6319° |
| argument of perigee: | 270.1585° |
| revolutions per day: | 15.27578997 |
| mean anomaly at epoch: | 89.9037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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