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 66343U 26145.46604883 +.00000000 +00000-0 +65860-3 0 00000
2 66343 43.0004 139.1536 0001779 274.3422 85.7226 15.27596144 05
| Epoch (UTC): | 25 May 2026 11:11:06 |
| Eccentricity: | 0.0001779 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.1536° |
| argument of perigee: | 274.3422° |
| revolutions per day: | 15.27596144 |
| mean anomaly at epoch: | 85.7226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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