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 66386U 26145.41329744 +.00000000 +00000-0 +64030-3 0 00000
2 66386 53.1586 220.4095 0000916 49.2067 310.9013 15.30198824 03
| Epoch (UTC): | 25 May 2026 09:55:08 |
| Eccentricity: | 0.0000916 |
| inclination: | 53.1586° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 220.4095° |
| argument of perigee: | 49.2067° |
| revolutions per day: | 15.30198824 |
| mean anomaly at epoch: | 310.9013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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