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 66488U 26145.66671028 +.00000000 +00000-0 +49659-3 0 00005
2 66488 43.0026 275.7894 0001081 273.8417 86.2312 15.27589385 08
| Epoch (UTC): | 25 May 2026 16:00:03 |
| Eccentricity: | 0.0001081 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 275.7894° |
| argument of perigee: | 273.8417° |
| revolutions per day: | 15.27589385 |
| mean anomaly at epoch: | 86.2312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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