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 66425U 26145.47241590 +.00000000 +00000-0 +38171-3 0 00009
2 66425 43.0042 200.7730 0002046 271.0483 89.0134 15.27587450 03
| Epoch (UTC): | 25 May 2026 11:20:16 |
| Eccentricity: | 0.0002046 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.7730° |
| argument of perigee: | 271.0483° |
| revolutions per day: | 15.27587450 |
| mean anomaly at epoch: | 89.0134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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