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 66870U 26040.31218050 +.00000000 +00000-0 +76236-3 0 00009
2 66870 42.9994 143.8926 0001709 270.0743 89.9913 15.27590117 06
| Epoch (UTC): | 09 February 2026 07:29:32 |
| Eccentricity: | 0.0001709 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 143.8926° |
| argument of perigee: | 270.0743° |
| revolutions per day: | 15.27590117 |
| mean anomaly at epoch: | 89.9913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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