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 66466U 26145.61452866 +.00000000 +00000-0 +24384-3 0 00001
2 66466 43.0005 221.5177 0001512 270.7565 89.3113 15.27583239 08
| Epoch (UTC): | 25 May 2026 14:44:55 |
| Eccentricity: | 0.0001512 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 221.5177° |
| argument of perigee: | 270.7565° |
| revolutions per day: | 15.27583239 |
| mean anomaly at epoch: | 89.3113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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