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 66171U 26145.19295691 +.00000000 +00000-0 +11756-2 0 00006
2 66171 53.1594 66.5844 0001106 88.6151 271.4979 15.34410837 05
| Epoch (UTC): | 25 May 2026 04:37:51 |
| Eccentricity: | 0.0001106 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 66.5844° |
| argument of perigee: | 88.6151° |
| revolutions per day: | 15.34410837 |
| mean anomaly at epoch: | 271.4979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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