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 66442U 26145.43658500 +.00000000 +00000-0 +59107-3 0 00009
2 66442 42.9994 201.3553 0001396 281.0187 79.0507 15.27594911 08
| Epoch (UTC): | 25 May 2026 10:28:40 |
| Eccentricity: | 0.0001396 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 201.3553° |
| argument of perigee: | 281.0187° |
| revolutions per day: | 15.27594911 |
| mean anomaly at epoch: | 79.0507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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