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 20066U 26145.32843654 +.00000000 +00000-0 +00000-0 0 00000
2 20066 12.9237 341.7964 0001546 299.1868 230.9973 0.98822346 08
| Epoch (UTC): | 25 May 2026 07:52:56 |
| Eccentricity: | 0.0001546 |
| inclination: | 12.9237° |
| perigee height: | 36191 km |
| apogee height: | 36204 km |
| right ascension of ascending node: | 341.7964° |
| argument of perigee: | 299.1868° |
| revolutions per day: | 0.98822346 |
| mean anomaly at epoch: | 230.9973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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