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 66794U 26145.43342183 +.00000000 +00000-0 +53147-3 0 00004
2 66794 43.0003 41.1716 0000235 324.7288 35.3548 15.27591753 01
| Epoch (UTC): | 25 May 2026 10:24:07 |
| Eccentricity: | 0.0000235 |
| inclination: | 43.0003° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 41.1716° |
| argument of perigee: | 324.7288° |
| revolutions per day: | 15.27591753 |
| mean anomaly at epoch: | 35.3548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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