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 66345U 26145.32499559 +.00000000 +00000-0 +52016-3 0 00008
2 66345 43.0000 139.8087 0001515 267.3037 92.7641 15.27594695 01
| Epoch (UTC): | 25 May 2026 07:47:59 |
| Eccentricity: | 0.0001515 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.8087° |
| argument of perigee: | 267.3037° |
| revolutions per day: | 15.27594695 |
| mean anomaly at epoch: | 92.7641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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