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 66534U 26145.48226061 +.00000000 +00000-0 +23554-3 0 00006
2 66534 43.0036 204.6143 0001466 267.3738 92.6946 15.27580386 06
| Epoch (UTC): | 25 May 2026 11:34:27 |
| Eccentricity: | 0.0001466 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.6143° |
| argument of perigee: | 267.3738° |
| revolutions per day: | 15.27580386 |
| mean anomaly at epoch: | 92.6946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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