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 57061U 26145.05765645 +.00000000 +00000-0 +40837-4 0 00004
2 57061 43.0046 42.6243 0000882 247.6286 112.4473 15.27582441 03
| Epoch (UTC): | 25 May 2026 01:23:01 |
| Eccentricity: | 0.0000882 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 42.6243° |
| argument of perigee: | 247.6286° |
| revolutions per day: | 15.27582441 |
| mean anomaly at epoch: | 112.4473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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