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 66601U 26145.23805566 +.00000000 +00000-0 +62055-3 0 00006
2 66601 42.9972 343.8216 0001442 263.6758 96.3930 15.27586070 00
| Epoch (UTC): | 25 May 2026 05:42:48 |
| Eccentricity: | 0.0001442 |
| inclination: | 42.9972° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 343.8216° |
| argument of perigee: | 263.6758° |
| revolutions per day: | 15.27586070 |
| mean anomaly at epoch: | 96.3930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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