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 66482U 26145.55684867 +.00000000 +00000-0 +51995-3 0 00008
2 66482 43.0002 221.9345 0001789 270.3444 89.7202 15.27606856 06
| Epoch (UTC): | 25 May 2026 13:21:51 |
| Eccentricity: | 0.0001789 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 221.9345° |
| argument of perigee: | 270.3444° |
| revolutions per day: | 15.27606856 |
| mean anomaly at epoch: | 89.7202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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