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 13066U 26071.79561188 +.00000000 +00000-0 +67993-4 0 00008
2 13066 82.9017 352.5481 0042600 311.5936 101.9980 13.77379758 08
| Epoch (UTC): | 12 March 2026 19:05:40 |
| Eccentricity: | 0.0042600 |
| inclination: | 82.9017° |
| perigee height: | 942 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 352.5481° |
| argument of perigee: | 311.5936° |
| revolutions per day: | 13.77379758 |
| mean anomaly at epoch: | 101.9980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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