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 66572U 26144.78263029 +.00000000 +00000-0 +80670-3 0 00007
2 66572 43.0004 277.6432 0001537 273.8714 86.1962 15.27554131 04
| Epoch (UTC): | 24 May 2026 18:46:59 |
| Eccentricity: | 0.0001537 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.6432° |
| argument of perigee: | 273.8714° |
| revolutions per day: | 15.27554131 |
| mean anomaly at epoch: | 86.1962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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