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 66857U 26145.39718513 +.00000000 +00000-0 +60385-3 0 00005
2 66857 43.0021 270.5598 0002051 269.0924 90.9693 15.27591782 03
| Epoch (UTC): | 25 May 2026 09:31:56 |
| Eccentricity: | 0.0002051 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.5598° |
| argument of perigee: | 269.0924° |
| revolutions per day: | 15.27591782 |
| mean anomaly at epoch: | 90.9693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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