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 26066.02162130 +.00000000 +00000-0 +11241-3 0 00008
2 06660 81.2335 161.8944 0047501 140.1752 220.2919 14.06268786 05
| Epoch (UTC): | 07 March 2026 00:31:08 |
| Eccentricity: | 0.0047501 |
| inclination: | 81.2335° |
| perigee height: | 838 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 161.8944° |
| argument of perigee: | 140.1752° |
| revolutions per day: | 14.06268786 |
| mean anomaly at epoch: | 220.2919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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