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 66001U 26145.56117622 +.00000000 +00000-0 +44962-4 0 00003
2 66001 50.0023 256.5991 0000930 151.6988 208.3935 13.29327451 09
| Epoch (UTC): | 25 May 2026 13:28:05 |
| Eccentricity: | 0.0000930 |
| inclination: | 50.0023° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 256.5991° |
| argument of perigee: | 151.6988° |
| revolutions per day: | 13.29327451 |
| mean anomaly at epoch: | 208.3935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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