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 66502U 26144.72189757 +.00000000 +00000-0 +56086-3 0 00003
2 66502 42.9998 281.5989 0001422 273.7166 86.3523 15.27588191 09
| Epoch (UTC): | 24 May 2026 17:19:31 |
| Eccentricity: | 0.0001422 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 281.5989° |
| argument of perigee: | 273.7166° |
| revolutions per day: | 15.27588191 |
| mean anomaly at epoch: | 86.3523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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