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 57529U 26145.45380075 +.00000000 +00000-0 +52146-4 0 00003
2 57529 43.0032 287.8838 0001782 269.1688 90.8960 15.27580414 03
| Epoch (UTC): | 25 May 2026 10:53:28 |
| Eccentricity: | 0.0001782 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 287.8838° |
| argument of perigee: | 269.1688° |
| revolutions per day: | 15.27580414 |
| mean anomaly at epoch: | 90.8960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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