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 66845U 26145.42594689 +.00000000 +00000-0 +31692-4 0 00002
2 66845 70.0008 140.8388 0003896 263.3239 96.7476 14.98336229 08
| Epoch (UTC): | 25 May 2026 10:13:21 |
| Eccentricity: | 0.0003896 |
| inclination: | 70.0008° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 140.8388° |
| argument of perigee: | 263.3239° |
| revolutions per day: | 14.98336229 |
| mean anomaly at epoch: | 96.7476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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