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 66889U 26144.95632405 +.00000000 +00000-0 +77098-3 0 00005
2 66889 53.1605 29.7232 0001146 84.0899 276.0234 15.34392350 03
| Epoch (UTC): | 24 May 2026 22:57:06 |
| Eccentricity: | 0.0001146 |
| inclination: | 53.1605° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 29.7232° |
| argument of perigee: | 84.0899° |
| revolutions per day: | 15.34392350 |
| mean anomaly at epoch: | 276.0234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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