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 66541U 26145.52837705 +.00000000 +00000-0 +64559-3 0 00002
2 66541 43.0001 204.0983 0001537 278.0949 81.9729 15.27596616 07
| Epoch (UTC): | 25 May 2026 12:40:51 |
| Eccentricity: | 0.0001537 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.0983° |
| argument of perigee: | 278.0949° |
| revolutions per day: | 15.27596616 |
| mean anomaly at epoch: | 81.9729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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