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 66329U 26145.44805669 +.00000000 +00000-0 +55565-3 0 00008
2 66329 43.0008 139.0212 0002376 282.1708 77.8877 15.27592417 04
| Epoch (UTC): | 25 May 2026 10:45:12 |
| Eccentricity: | 0.0002376 |
| inclination: | 43.0008° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 139.0212° |
| argument of perigee: | 282.1708° |
| revolutions per day: | 15.27592417 |
| mean anomaly at epoch: | 77.8877° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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