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 66537U 26145.52194803 +.00000000 +00000-0 +89351-4 0 00000
2 66537 43.0007 204.0494 0001624 278.4501 81.6167 15.27567181 08
| Epoch (UTC): | 25 May 2026 12:31:36 |
| Eccentricity: | 0.0001624 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.0494° |
| argument of perigee: | 278.4501° |
| revolutions per day: | 15.27567181 |
| mean anomaly at epoch: | 81.6167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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