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 57818U 26145.51332053 +.00000000 +00000-0 +34618-4 0 00008
2 57818 43.0013 160.6438 0001366 268.4578 91.6117 15.27578959 09
| Epoch (UTC): | 25 May 2026 12:19:10 |
| Eccentricity: | 0.0001366 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 160.6438° |
| argument of perigee: | 268.4578° |
| revolutions per day: | 15.27578959 |
| mean anomaly at epoch: | 91.6117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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