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 66428U 26145.59291331 +.00000000 +00000-0 +66959-3 0 00008
2 66428 43.0020 199.9542 0001459 269.9249 90.1435 15.27582883 07
| Epoch (UTC): | 25 May 2026 14:13:47 |
| Eccentricity: | 0.0001459 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 199.9542° |
| argument of perigee: | 269.9249° |
| revolutions per day: | 15.27582883 |
| mean anomaly at epoch: | 90.1435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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