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 66439U 26145.43900811 +.00000000 +00000-0 +52025-3 0 00002
2 66439 42.9991 200.5107 0001317 280.5946 79.4757 15.27593208 06
| Epoch (UTC): | 25 May 2026 10:32:10 |
| Eccentricity: | 0.0001317 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.5107° |
| argument of perigee: | 280.5946° |
| revolutions per day: | 15.27593208 |
| mean anomaly at epoch: | 79.4757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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