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 06660U 26071.71361112 +.00000000 +00000-0 +29828-4 0 00002
2 06660 81.2333 156.3826 0047897 124.2491 236.3228 14.06270256 08
| Epoch (UTC): | 12 March 2026 17:07:36 |
| Eccentricity: | 0.0047897 |
| inclination: | 81.2333° |
| perigee height: | 837 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 156.3826° |
| argument of perigee: | 124.2491° |
| revolutions per day: | 14.06270256 |
| mean anomaly at epoch: | 236.3228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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