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 26070.93096319 +.00000000 +00000-0 +35012-4 0 00001
2 06660 81.2334 157.1405 0047850 126.4216 234.1380 14.06270096 06
| Epoch (UTC): | 11 March 2026 22:20:35 |
| Eccentricity: | 0.0047850 |
| inclination: | 81.2334° |
| perigee height: | 837 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 157.1405° |
| argument of perigee: | 126.4216° |
| revolutions per day: | 14.06270096 |
| mean anomaly at epoch: | 234.1380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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