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 66431U 26145.45185823 +.00000000 +00000-0 +35134-3 0 00006
2 66431 42.9984 200.6124 0001479 274.1472 85.9210 15.27583832 00
| Epoch (UTC): | 25 May 2026 10:50:40 |
| Eccentricity: | 0.0001479 |
| inclination: | 42.9984° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.6124° |
| argument of perigee: | 274.1472° |
| revolutions per day: | 15.27583832 |
| mean anomaly at epoch: | 85.9210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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