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 66438U 26145.47369828 +.00000000 +00000-0 +31663-3 0 00007
2 66438 43.0047 200.7754 0001881 270.2283 89.8353 15.27587114 01
| Epoch (UTC): | 25 May 2026 11:22:07 |
| Eccentricity: | 0.0001881 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.7754° |
| argument of perigee: | 270.2283° |
| revolutions per day: | 15.27587114 |
| mean anomaly at epoch: | 89.8353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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